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Wikipedia

Airplane

An airplane (American English), or aeroplane (Commonwealth English), informally plane, is a fixed-wing aircraft that is propelled forward by thrust from a jet engine, propeller, or rocket engine. Airplanes come in a variety of sizes, shapes, and wing configurations. The broad spectrum of uses for airplanes includes recreation, transportation of goods and people, military, and research. Worldwide, commercial aviation transports more than four billion passengers annually on airliners[1] and transports more than 200 billion tonne-kilometers[2] of cargo annually, which is less than 1% of the world's cargo movement.[3] Most airplanes are flown by a pilot on board the aircraft, but some are designed to be remotely or computer-controlled such as drones.

The first flight of an airplane, the Wright Flyer on December 17, 1903

The Wright brothers invented and flew the first airplane in 1903, recognized as "the first sustained and controlled heavier-than-air powered flight".[4] They built on the works of George Cayley dating from 1799, when he set forth the concept of the modern airplane (and later built and flew models and successful passenger-carrying gliders)[5] and the work of German pioneer of human aviation Otto Lilienthal, who, between 1867 and 1896, also studied heavier-than-air flight. Lilienthal's flight attempts in 1891 are seen as the beginning of human flight.[6] Following its limited use in World War I, aircraft technology continued to develop. Airplanes had a presence in all the major battles of World War II. The first jet aircraft was the German Heinkel He 178 in 1939. The first jet airliner, the de Havilland Comet, was introduced in 1952. The Boeing 707, the first widely successful commercial jet, was in commercial service for more than 50 years, from 1958 to at least 2013.

Etymology and usage

First attested in English in the late 19th century (prior to the first sustained powered flight), the word airplane, like aeroplane, derives from the French aéroplane, which comes from the Greek ἀήρ (aēr), "air"[7] and either Latin planus, "level",[8] or Greek πλάνος (planos), "wandering".[9][10] "Aéroplane" originally referred just to the wing, as it is a plane moving through the air.[11] In an example of synecdoche, the word for the wing came to refer to the entire aircraft.

In the United States and Canada, the term "airplane" is used for powered fixed-wing aircraft. In the United Kingdom and Ireland and most of the Commonwealth, the term "aeroplane" (/ˈɛərəpln/[11]) is usually applied to these aircraft.

History

 
Le Bris and his glider, Albatros II, photographed by Nadar, 1868
 
Otto Lilienthal in mid-flight, c. 1895

Antecedents

Many stories from antiquity involve flight, such as the Greek legend of Icarus and Daedalus, and the Vimana in ancient Indian epics. Around 400 BC in Greece, Archytas was reputed to have designed and built the first artificial, self-propelled flying device, a bird-shaped model propelled by a jet of what was probably steam, said to have flown some 200 m (660 ft).[12][13] This machine may have been suspended for its flight.[14][15]

Some of the earliest recorded attempts with gliders were those by the 9th-century Andalusian and Arabic-language poet Abbas ibn Firnas and the 11th-century English monk Eilmer of Malmesbury; both experiments injured their pilots.[16] Leonardo da Vinci researched the wing design of birds and designed a man-powered aircraft in his Codex on the Flight of Birds (1502), noting for the first time the distinction between the center of mass and the center of pressure of flying birds.

In 1799, George Cayley set forth the concept of the modern airplane as a fixed-wing flying machine with separate systems for lift, propulsion, and control.[17][18] Cayley was building and flying models of fixed-wing aircraft as early as 1803, and he built a successful passenger-carrying glider in 1853.[5] In 1856, Frenchman Jean-Marie Le Bris made the first powered flight, by having his glider "L'Albatros artificiel" pulled by a horse on a beach.[19] Then the Russian Alexander F. Mozhaisky also made some innovative designs. In 1883, the American John J. Montgomery made a controlled flight in a glider.[20] Other aviators who made similar flights at that time were Otto Lilienthal, Percy Pilcher, and Octave Chanute.

Sir Hiram Maxim built a craft that weighed 3.5 tons, with a 110-foot (34 m) wingspan that was powered by two 360-horsepower (270 kW) steam engines driving two propellers. In 1894, his machine was tested with overhead rails to prevent it from rising. The test showed that it had enough lift to take off. The craft was uncontrollable and it is presumed that Maxim realized this because he subsequently abandoned work on it.[21]

In the 1890s, Lawrence Hargrave conducted research on wing structures and developed a box kite that lifted the weight of a man. His box kite designs were widely adopted. Although he also developed a type of rotary aircraft engine, he did not create and fly a powered fixed-wing aircraft.[22]

Between 1867 and 1896, the German pioneer of human aviation Otto Lilienthal developed heavier-than-air flight. He was the first person to make well-documented, repeated, successful gliding flights. Lilienthal's work led to him developing the concept of the modern wing,[23][24] his flight attempts in 1891 are seen as the beginning of human flight,[25] the "Lilienthal Normalsegelapparat" is considered to be the first airplane in series production and his work heavily inspired the Wright brothers.[26]

Early powered flights

 
Patent drawings of Clement Ader's Éole.

The Frenchman Clement Ader constructed his first of three flying machines in 1886, the Éole. It was a bat-like design run by a lightweight steam engine of his own invention, with four cylinders developing 20 horsepower (15 kW), driving a four-blade propeller. The engine weighed no more than 4 kilograms per kilowatt (6.6 lb/hp). The wings had a span of 14 m (46 ft). All-up weight was 300 kilograms (660 lb). On 9 October 1890, Ader attempted to fly the Éole. Aviation historians give credit to this effort as a powered take-off and uncontrolled hop of approximately 50 m (160 ft) at a height of approximately 200 mm (7.9 in).[27][28] Ader's two subsequent machines were not documented to have achieved flight.[29]

The American Wright brothers flights in 1903 are recognized by the Fédération Aéronautique Internationale (FAI), the standard-setting and record-keeping body for aeronautics, as "the first sustained and controlled heavier-than-air powered flight".[4] By 1905, the Wright Flyer III was capable of fully controllable, stable flight for substantial periods. The Wright brothers credited Otto Lilienthal as a major inspiration for their decision to pursue manned flight.

 
Santos-Dumont 14-bis, between 1906 and 1907

In 1906, the Brazilian Alberto Santos-Dumont made what was claimed to be the first airplane flight unassisted by catapult[30] and set the first world record recognized by the Aéro-Club de France by flying 220 meters (720 ft) in less than 22 seconds.[31] This flight was also certified by the FAI.[32][33]

An early aircraft design that brought together the modern monoplane tractor configuration was the Blériot VIII design of 1908. It had movable tail surfaces controlling both yaw and pitch, a form of roll control supplied either by wing warping or by ailerons and controlled by its pilot with a joystick and rudder bar. It was an important predecessor of his later Blériot XI Channel-crossing aircraft of the summer of 1909.[34]

World War I served as a testbed for the use of the airplane as a weapon. Airplanes demonstrated their potential as mobile observation platforms, then proved themselves to be machines of war capable of causing casualties to the enemy. The earliest known aerial victory with a synchronized machine gun-armed fighter aircraft occurred in 1915, by German Luftstreitkräfte Leutnant Kurt Wintgens. Fighter aces appeared; the greatest (by number of Aerial Combat victories) was Manfred von Richthofen.

Following WWI, aircraft technology continued to develop. Alcock and Brown crossed the Atlantic non-stop for the first time in 1919. The first international commercial flights took place between the United States and Canada in 1919.[35]

Airplanes had a presence in all the major battles of World War II. They were an essential component of the military strategies of the period, such as the German Blitzkrieg, The Battle of Britain, and the American and Japanese aircraft carrier campaigns of the Pacific War.

Development of jet aircraft

 
The Concorde supersonic transport aircraft

The first practical jet aircraft was the German Heinkel He 178, which was tested in 1939. In 1943, the Messerschmitt Me 262, the first operational jet fighter aircraft, went into service in the German Luftwaffe.

The first jet airliner, the de Havilland Comet, was introduced in 1952. The Boeing 707, the first widely successful commercial jet, was in commercial service for more than 50 years, from 1958 to 2010. The Boeing 747 was the world's biggest passenger aircraft from 1970 until it was surpassed by the Airbus A380 in 2005.

Supersonic airliner flights, including those of the Concorde, have been limited to over-water flight at supersonic speed because of their sonic boom, which is prohibited over most populated land areas. The high cost of operation per passenger-mile and a deadly crash in 2000 induced the operators of the Concorde to remove it from service.[36][37]

Propulsion

Propeller

An aircraft propeller, or airscrew, converts rotary motion from an engine or other power source, into a swirling slipstream which pushes the propeller forwards or backwards. It comprises a rotating power-driven hub, to which are attached two or more radial airfoil-section blades such that the whole assembly rotates about a longitudinal axis.[38] Three types of aviation engines used to power propellers include reciprocating engines (or piston engines), gas turbines, and electric motors. The amount of thrust a propeller creates is determined, in part, by its disk area—the area through which the blades rotate. The limitation on blade speed is the speed of sound; as when the blade tip exceeds the speed of sound, shock waves decrease propeller efficiency. The rpm required to generate a given tip speed is inversely proportional to the diameter of the propeller. The upper design speed limit for propeller-driven aircraft is Mach 0.6. Aircraft designed to go faster than that employ jet engines.[39]

Reciprocating engine

Reciprocating engines in aircraft have three main variants, radial, in-line and flat or horizontally opposed engine. The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders "radiate" outward from a central crankcase like the spokes of a wheel and was commonly used for aircraft engines before gas turbine engines became predominant. An inline engine is a reciprocating engine with banks of cylinders, one behind another, rather than rows of cylinders, with each bank having any number of cylinders, but rarely more than six, and may be water-cooled. A flat engine is an internal combustion engine with horizontally-opposed cylinders.

Gas turbine

A turboprop gas turbine engine consists of an intake, compressor, combustor, turbine, and a propelling nozzle, which provide power from a shaft through a reduction gearing to the propeller. The propelling nozzle provides a relatively small proportion of the thrust generated by a turboprop.

Electric motor

 
Solar Impulse 1, a solar-powered aircraft with electric motors.

An electric aircraft runs on electric motors with electricity coming from fuel cells, solar cells, ultracapacitors, power beaming,[40] or batteries. Currently, flying electric aircraft are mostly experimental prototypes, including manned and unmanned aerial vehicles, but there are some production models on the market.[41]

Jet

Jet aircraft are propelled by jet engines, which are used because the aerodynamic limitations of propellers do not apply to jet propulsion. These engines are much more powerful than a reciprocating engine for a given size or weight and are comparatively quiet and work well at higher altitude. Variants of the jet engine include the ramjet and the scramjet, which rely on high airspeed and intake geometry to compress the combustion air, prior to the introduction and ignition of fuel. Rocket motors provide thrust by burning a fuel with an oxidizer and expelling gas through a nozzle.

Turbofan

Most jet aircraft use turbofan jet engines, which employ a gas turbine to drive a ducted fan, which accelerates air around the turbine to provide thrust in addition to that which is accelerated through the turbine. The ratio of air passing around the turbine to that passing through is called the by-pass ratio.[42] They represent a compromise between turbojet (with no bypass) and turboprop forms of aircraft propulsion (primarily powered with bypass air).[43]

Subsonic aircraft, such as airliners, employ high by-pass jet engines for fuel efficiency. Supersonic aircraft, such as jet fighters, use low-bypass turbofans. However at supersonic speeds, the air entering the engine must be decelerated to a subsonic speed and then re-accelerated back to supersonic speeds after combustion. An afterburner may be used on combat aircraft to increase power for short periods of time by injecting fuel directly into the hot exhaust gases. Many jet aircraft also use thrust reversers to slow down after landing.[43]

Ramjet

 
Artist's concept of X-43A with scramjet attached to the underside

A ramjet is a form of jet engine that contains no major moving parts and can be particularly useful in applications requiring a small and simple engine for high-speed use, such as with missiles. Ramjets require forward motion before they can generate thrust and so are often used in conjunction with other forms of propulsion, or with an external means of achieving sufficient speed. The Lockheed D-21 was a Mach 3+ ramjet-powered reconnaissance drone that was launched from a parent aircraft. A ramjet uses the vehicle's forward motion to force air through the engine without resorting to turbines or vanes. Fuel is added and ignited, which heats and expands the air to provide thrust.[44]

Scramjet

A scramjet is a specialized ramjet that uses internal supersonic airflow to compress, combine with fuel, combust and accelerate the exhaust to provide thrust. The engine operates at supersonic speeds only. The NASA X-43, an experimental unmanned scramjet, set a world speed record in 2004 for a jet-powered aircraft with a speed of Mach 9.7, nearly 12,100 kilometers per hour (7,500 mph).[45]

Rocket

 
Bell X-1 in flight, 1947

Whereas jet aircraft use the atmosphere both as a source of oxidant and of mass to accelerate reactively behind the aircraft, rocket aircraft carry the oxidizer on board and accelerate the burned fuel and oxidizer backwards as the sole source of mass for reaction. Liquid fuel and oxidizer may be pumped into a combustion chamber or a solid fuel with oxidizer may burn in the fuel chamber. Whether liquid or solid-fueled, the hot gas is accelerated through a nozzle.[46]

In World War II, the Germans deployed the Me 163 Komet rocket-powered aircraft. The first plane to break the sound barrier in level flight was a rocket plane – the Bell X-1 in 1948. The North American X-15 broke many speed and altitude records in the 1960s and pioneered engineering concepts for later aircraft and spacecraft. Military transport aircraft may employ rocket-assisted take offs for short-field situations. Otherwise, rocket aircraft include spaceplanes, like SpaceShipTwo, for travel beyond the Earth's atmosphere and sport aircraft developed for the short-lived Rocket Racing League.

Design and manufacture

 
Assembly line of the SR-71 Blackbird at Skunk Works, Lockheed Martin’s Advanced Development Programs (ADP).

Most airplanes are constructed by companies with the objective of producing them in quantity for customers. The design and planning process, including safety tests, can last up to four years for small turboprops or longer for larger planes.

During this process, the objectives and design specifications of the aircraft are established. First the construction company uses drawings and equations, simulations, wind tunnel tests and experience to predict the behavior of the aircraft. Computers are used by companies to draw, plan and do initial simulations of the aircraft. Small models and mockups of all or certain parts of the plane are then tested in wind tunnels to verify its aerodynamics.

When the design has passed through these processes, the company constructs a limited number of prototypes for testing on the ground. Representatives from an aviation governing agency often make a first flight. The flight tests continue until the aircraft has fulfilled all the requirements. Then, the governing public agency of aviation of the country authorizes the company to begin production.

In the United States, this agency is the Federal Aviation Administration (FAA). In the European Union, European Aviation Safety Agency (EASA); in the United Kingdom it is the Civil Aviation Authority (CAA).[47] In Canada, the public agency in charge and authorizing the mass production of aircraft is Transport Canada's Civil Aviation Authority.[48]

When a part or component needs to be joined together by welding for virtually any aerospace or defense application, it must meet the most stringent and specific safety regulations and standards. Nadcap, or the National Aerospace and Defense Contractors Accreditation Program sets global requirements for quality, quality management and quality assurance for aerospace engineering.[49]

In the case of international sales, a license from the public agency of aviation or transport of the country where the aircraft is to be used is also necessary. For example, airplanes made by the European company, Airbus, need to be certified by the FAA to be flown in the United States, and airplanes made by U.S.-based Boeing need to be approved by the EASA to be flown in the European Union.[50]

Regulations have resulted in reduced noise from aircraft engines in response to increased noise pollution from growth in air traffic over urban areas near airports.[51]

Small planes can be designed and constructed by amateurs as homebuilts. Other homebuilt aircraft can be assembled using pre-manufactured kits of parts that can be assembled into a basic plane and must then be completed by the builder.[52]

Few companies produce planes on a large scale. However, the production of a plane for one company is a process that actually involves dozens, or even hundreds, of other companies and plants, that produce the parts that go into the plane. For example, one company can be responsible for the production of the landing gear, while another one is responsible for the radar. The production of such parts is not limited to the same city or country; in the case of large plane manufacturing companies, such parts can come from all over the world.[citation needed]

The parts are sent to the main plant of the plane company, where the production line is located. In the case of large planes, production lines dedicated to the assembly of certain parts of the plane can exist, especially the wings and the fuselage.[citation needed]

When complete, a plane is rigorously inspected to search for imperfections and defects. After approval by inspectors, the plane is put through a series of flight tests to assure that all systems are working correctly and that the plane handles properly. Upon passing these tests, the plane is ready to receive the "final touchups" (internal configuration, painting, etc.), and is then ready for the customer.[citation needed]

Characteristics

 
Major components of an airplane.
 
An IAI Heron - an unmanned aerial vehicle with a twin-boom configuration

Airframe

The structural parts of a fixed-wing aircraft are called the airframe. The parts present can vary according to the aircraft's type and purpose. Early types were usually made of wood with fabric wing surfaces, When engines became available for powered flight around a hundred years ago, their mounts were made of metal. Then as speeds increased more and more parts became metal until by the end of WWII all-metal aircraft were common. In modern times, increasing use of composite materials has been made.

Typical structural parts include:

  • One or more large horizontal wings, often with an airfoil cross-section shape. The wing deflects air downward as the aircraft moves forward, generating lifting force to support it in flight. The wing also provides stability in roll to stop the aircraft from rolling to the left or right in steady flight.
 
The An-225 Mriya, which could carry a 250-tonne payload, had two vertical stabilizers.
  • A fuselage, a long, thin body, usually with tapered or rounded ends to make its shape aerodynamically smooth. The fuselage joins the other parts of the airframe and usually contains important things such as the pilot, payload and flight systems.
  • A vertical stabilizer or fin is a vertical wing-like surface mounted at the rear of the plane and typically protruding above it. The fin stabilizes the plane's yaw (turn left or right) and mounts the rudder, which controls its rotation along that axis.
  • A horizontal stabilizer or tailplane, usually mounted at the tail near the vertical stabilizer. The horizontal stabilizer is used to stabilize the plane's pitch (tilt up or down) and mounts the elevators, which provide pitch control.
  • Landing gear, a set of wheels, skids, or floats that support the plane while it is on the surface. On seaplanes, the bottom of the fuselage or floats (pontoons) support it while on the water. On some planes the landing gear retracts during flight to reduce drag.

Wings

The wings of a fixed-wing aircraft are static planes extending either side of the aircraft. When the aircraft travels forwards, air flows over the wings, which are shaped to create lift. This shape is called an airfoil and is shaped like a bird's wing.

Wing structure

Airplanes have flexible wing surfaces which are stretched across a frame and made rigid by the lift forces exerted by the airflow over them. Larger aircraft have rigid wing surfaces which provide additional strength.

Whether flexible or rigid, most wings have a strong frame to give them their shape and to transfer lift from the wing surface to the rest of the aircraft. The main structural elements are one or more spars running from root to tip, and many ribs running from the leading (front) to the trailing (rear) edge.

Early airplane engines had little power, and lightness was very important. Also, early airfoil sections were very thin, and could not have a strong frame installed within. So, until the 1930s, most wings were too lightweight to have enough strength, and external bracing struts and wires were added. When the available engine power increased during the 1920s and 30s, wings could be made heavy and strong enough that bracing was not needed any more. This type of unbraced wing is called a cantilever wing.

Wing configuration

 
Captured Morane-Saulnier L wire-braced parasol monoplane

The number and shape of the wings varies widely on different types. A given wing plane may be full-span or divided by a central fuselage into port (left) and starboard (right) wings. Occasionally, even more wings have been used, with the three-winged triplane achieving some fame in WWI. The four-winged quadruplane and other multiplane designs have had little success.

A monoplane has a single wing plane, a biplane has two stacked one above the other, a tandem wing has two placed one behind the other. When the available engine power increased during the 1920s and 30s and bracing was no longer needed, the unbraced or cantilever monoplane became the most common form of powered type.

The wing planform is the shape when seen from above. To be aerodynamically efficient, a wing should be straight with a long span from side to side but have a short chord (high aspect ratio). But to be structurally efficient, and hence light weight, a wing must have a short span but still enough area to provide lift (low aspect ratio).

At transonic speeds (near the speed of sound), it helps to sweep the wing backwards or forwards to reduce drag from supersonic shock waves as they begin to form. The swept wing is just a straight wing swept backwards or forwards.

 
Two Dassault Mirage G prototypes, one with wings swept

The delta wing is a triangle shape that may be used for several reasons. As a flexible Rogallo wing, it allows a stable shape under aerodynamic forces and so is often used for ultralight aircraft and even kites. As a supersonic wing, it combines high strength with low drag and so is often used for fast jets.

A variable geometry wing can be changed in flight to a different shape. The variable-sweep wing transforms between an efficient straight configuration for takeoff and landing, to a low-drag swept configuration for high-speed flight. Other forms of variable planform have been flown, but none have gone beyond the research stage.

Fuselage

A fuselage is a long, thin body, usually with tapered or rounded ends to make its shape aerodynamically smooth. The fuselage may contain the flight crew, passengers, cargo or payload, fuel and engines. The pilots of manned aircraft operate them from a cockpit located at the front or top of the fuselage and equipped with controls and usually windows and instruments. A plane may have more than one fuselage, or it may be fitted with booms with the tail located between the booms to allow the extreme rear of the fuselage to be useful for a variety of purposes.

Wings vs. bodies

Flying wing

 
The US-produced B-2 Spirit is a strategic bomber. It has a flying wing configuration and is capable of intercontinental missions

A flying wing is a tailless aircraft which has no definite fuselage. Most of the crew, payload and equipment are housed inside the main wing structure.[53]

The flying wing configuration was studied extensively in the 1930s and 1940s, notably by Jack Northrop and Cheston L. Eshelman in the United States, and Alexander Lippisch and the Horten brothers in Germany. After the war, several experimental designs were based on the flying wing concept, but the known difficulties remained intractable. Some general interest continued until the early 1950s but designs did not necessarily offer a great advantage in range and presented several technical problems, leading to the adoption of "conventional" solutions like the Convair B-36 and the B-52 Stratofortress. Due to the practical need for a deep wing, the flying wing concept is most practical for designs in the slow-to-medium speed range, and there has been continual interest in using it as a tactical airlifter design.

Interest in flying wings was renewed in the 1980s due to their potentially low radar reflection cross-sections. Stealth technology relies on shapes which only reflect radar waves in certain directions, thus making the aircraft hard to detect unless the radar receiver is at a specific position relative to the aircraft - a position that changes continuously as the aircraft moves. This approach eventually led to the Northrop B-2 Spirit stealth bomber. In this case, the aerodynamic advantages of the flying wing are not the primary needs. However, modern computer-controlled fly-by-wire systems allowed for many of the aerodynamic drawbacks of the flying wing to be minimized, making for an efficient and stable long-range bomber.

Blended wing body

 
Computer-generated model of the Boeing X-48

Blended wing body aircraft have a flattened and airfoil shaped body, which produces most of the lift to keep itself aloft, and distinct and separate wing structures, though the wings are smoothly blended in with the body.

Thus blended wing bodied aircraft incorporate design features from both a futuristic fuselage and flying wing design. The purported advantages of the blended wing body approach are efficient high-lift wings and a wide airfoil-shaped body. This enables the entire craft to contribute to lift generation with the result of potentially increased fuel economy.

Lifting body

 
The Martin Aircraft Company X-24 was built as part of a 1963 to 1975 experimental US military program.

A lifting body is a configuration in which the body itself produces lift. In contrast to a flying wing, which is a wing with minimal or no conventional fuselage, a lifting body can be thought of as a fuselage with little or no conventional wing. Whereas a flying wing seeks to maximize cruise efficiency at subsonic speeds by eliminating non-lifting surfaces, lifting bodies generally minimize the drag and structure of a wing for subsonic, supersonic, and hypersonic flight, or, spacecraft re-entry. All of these flight regimes pose challenges for proper flight stability. Lifting bodies were a major area of research in the 1960s and 70s as a means to build a small and lightweight manned spacecraft. The US built several famous lifting body rocket planes to test the concept, as well as several rocket-launched re-entry vehicles that were tested over the Pacific. Interest waned as the US Air Force lost interest in the manned mission, and major development ended during the Space Shuttle design process when it became clear that the highly shaped fuselages made it difficult to fit fuel tankage.

Empennage and foreplane

 
Canards on the Saab Viggen

The classic airfoil section wing is unstable in flight and difficult to control. Flexible-wing types often rely on an anchor line or the weight of a pilot hanging beneath to maintain the correct attitude. Some free-flying types use an adapted airfoil that is stable, or other ingenious mechanisms including, most recently, electronic artificial stability.

To achieve stability and control, most fixed-wing types have an empennage comprising a fin and rudder which act horizontally and a tailplane and elevator which act vertically. These control surfaces can typically be trimmed to relieve control forces for various stages of flight. This is so common that it is known as the conventional layout. Sometimes there may be two or more fins, spaced out along the tailplane.

Some types have a horizontal "canard" foreplane ahead of the main wing, instead of behind it.[54][55][56] This foreplane may contribute to the lift, the trim, or control of the aircraft, or to several of these.

Controls and instruments

 
A light aircraft (Robin DR400/500) cockpit

Airplanes have complex flight control systems. The main controls allow the pilot to direct the aircraft in the air by controlling the attitude (roll, pitch and yaw) and engine thrust.

On manned aircraft, cockpit instruments provide information to the pilots, including flight data, engine output, navigation, communications and other aircraft systems that may be installed.

Safety

When risk is measured by deaths per passenger kilometer, air travel is approximately 10 times safer than travel by bus or rail. However, when using the deaths per journey statistic, air travel is significantly more dangerous than car, rail, or bus travel.[57] Air travel insurance is relatively expensive for this reason—insurers generally use the deaths per journey statistic.[58] There is a significant difference between the safety of airliners and that of smaller private planes, with the per-mile statistic indicating that airliners are 8.3 times safer than smaller planes.[59]

Environmental impact

 
Water vapor contrails left by high-altitude jet airliners. These may contribute to cirrus cloud formation.

Like all activities involving combustion, fossil-fuel-powered aircraft release soot and other pollutants into the atmosphere. Greenhouse gases such as carbon dioxide (CO2) are also produced. In addition, there are environmental impacts specific to airplanes: for instance,

  • Airplanes operating at high altitudes near the tropopause (mainly large jet airliners) emit aerosols and leave contrails, both of which can increase cirrus cloud formation – cloud cover may have increased by up to 0.2% since the birth of aviation.[60]
  • Airplanes operating at high altitudes near the tropopause can also release chemicals that interact with greenhouse gases at those altitudes, particularly nitrogen compounds, which interact with ozone, increasing ozone concentrations.[61][62]
  • Most light piston aircraft burn avgas, which contains tetraethyllead (TEL). Some lower-compression piston engines can operate on unleaded mogas and turbine engines and diesel engines – neither of which require lead – are used on some newer light aircraft. Some non-polluting light electric aircraft are already in production.

Another environmental impact of airplanes is noise pollution, mainly caused by aircraft taking off and landing.

See also

References

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Bibliography

  • Blatner, David. The Flying Book: Everything You've Ever Wondered About Flying On Airplanes. ISBN 0-8027-7691-4

External links

  • The Aeroplane centre
  • Airliners.net
  • Aerospaceweb.org

airplane, aeroplane, redirects, here, other, uses, disambiguation, aeroplane, disambiguation, airplane, american, english, aeroplane, commonwealth, english, informally, plane, fixed, wing, aircraft, that, propelled, forward, thrust, from, engine, propeller, ro. Aeroplane redirects here For other uses see Airplane disambiguation and Aeroplane disambiguation An airplane American English or aeroplane Commonwealth English informally plane is a fixed wing aircraft that is propelled forward by thrust from a jet engine propeller or rocket engine Airplanes come in a variety of sizes shapes and wing configurations The broad spectrum of uses for airplanes includes recreation transportation of goods and people military and research Worldwide commercial aviation transports more than four billion passengers annually on airliners 1 and transports more than 200 billion tonne kilometers 2 of cargo annually which is less than 1 of the world s cargo movement 3 Most airplanes are flown by a pilot on board the aircraft but some are designed to be remotely or computer controlled such as drones North American P 51 Mustang a World War II fighter aircraft The first flight of an airplane the Wright Flyer on December 17 1903 An All Nippon Airways Boeing 777 300ER taking off from New York JFK Airport The Wright brothers invented and flew the first airplane in 1903 recognized as the first sustained and controlled heavier than air powered flight 4 They built on the works of George Cayley dating from 1799 when he set forth the concept of the modern airplane and later built and flew models and successful passenger carrying gliders 5 and the work of German pioneer of human aviation Otto Lilienthal who between 1867 and 1896 also studied heavier than air flight Lilienthal s flight attempts in 1891 are seen as the beginning of human flight 6 Following its limited use in World War I aircraft technology continued to develop Airplanes had a presence in all the major battles of World War II The first jet aircraft was the German Heinkel He 178 in 1939 The first jet airliner the de Havilland Comet was introduced in 1952 The Boeing 707 the first widely successful commercial jet was in commercial service for more than 50 years from 1958 to at least 2013 Contents 1 Etymology and usage 2 History 2 1 Antecedents 2 2 Early powered flights 2 3 Development of jet aircraft 3 Propulsion 3 1 Propeller 3 1 1 Reciprocating engine 3 1 2 Gas turbine 3 1 3 Electric motor 3 2 Jet 3 2 1 Turbofan 3 2 2 Ramjet 3 2 3 Scramjet 3 2 4 Rocket 4 Design and manufacture 5 Characteristics 5 1 Airframe 5 2 Wings 5 2 1 Wing structure 5 2 2 Wing configuration 5 3 Fuselage 5 4 Wings vs bodies 5 4 1 Flying wing 5 4 2 Blended wing body 5 4 3 Lifting body 5 5 Empennage and foreplane 5 6 Controls and instruments 6 Safety 7 Environmental impact 8 See also 9 References 10 Bibliography 11 External linksEtymology and usageFirst attested in English in the late 19th century prior to the first sustained powered flight the word airplane like aeroplane derives from the French aeroplane which comes from the Greek ἀhr aer air 7 and either Latin planus level 8 or Greek planos planos wandering 9 10 Aeroplane originally referred just to the wing as it is a plane moving through the air 11 In an example of synecdoche the word for the wing came to refer to the entire aircraft In the United States and Canada the term airplane is used for powered fixed wing aircraft In the United Kingdom and Ireland and most of the Commonwealth the term aeroplane ˈ ɛer e p l eɪ n 11 is usually applied to these aircraft HistoryMain articles Aviation history and First flying machine Le Bris and his glider Albatros II photographed by Nadar 1868 Otto Lilienthal in mid flight c 1895 Antecedents Many stories from antiquity involve flight such as the Greek legend of Icarus and Daedalus and the Vimana in ancient Indian epics Around 400 BC in Greece Archytas was reputed to have designed and built the first artificial self propelled flying device a bird shaped model propelled by a jet of what was probably steam said to have flown some 200 m 660 ft 12 13 This machine may have been suspended for its flight 14 15 Some of the earliest recorded attempts with gliders were those by the 9th century Andalusian and Arabic language poet Abbas ibn Firnas and the 11th century English monk Eilmer of Malmesbury both experiments injured their pilots 16 Leonardo da Vinci researched the wing design of birds and designed a man powered aircraft in his Codex on the Flight of Birds 1502 noting for the first time the distinction between the center of mass and the center of pressure of flying birds In 1799 George Cayley set forth the concept of the modern airplane as a fixed wing flying machine with separate systems for lift propulsion and control 17 18 Cayley was building and flying models of fixed wing aircraft as early as 1803 and he built a successful passenger carrying glider in 1853 5 In 1856 Frenchman Jean Marie Le Bris made the first powered flight by having his glider L Albatros artificiel pulled by a horse on a beach 19 Then the Russian Alexander F Mozhaisky also made some innovative designs In 1883 the American John J Montgomery made a controlled flight in a glider 20 Other aviators who made similar flights at that time were Otto Lilienthal Percy Pilcher and Octave Chanute Sir Hiram Maxim built a craft that weighed 3 5 tons with a 110 foot 34 m wingspan that was powered by two 360 horsepower 270 kW steam engines driving two propellers In 1894 his machine was tested with overhead rails to prevent it from rising The test showed that it had enough lift to take off The craft was uncontrollable and it is presumed that Maxim realized this because he subsequently abandoned work on it 21 In the 1890s Lawrence Hargrave conducted research on wing structures and developed a box kite that lifted the weight of a man His box kite designs were widely adopted Although he also developed a type of rotary aircraft engine he did not create and fly a powered fixed wing aircraft 22 Between 1867 and 1896 the German pioneer of human aviation Otto Lilienthal developed heavier than air flight He was the first person to make well documented repeated successful gliding flights Lilienthal s work led to him developing the concept of the modern wing 23 24 his flight attempts in 1891 are seen as the beginning of human flight 25 the Lilienthal Normalsegelapparat is considered to be the first airplane in series production and his work heavily inspired the Wright brothers 26 Early powered flights Patent drawings of Clement Ader s Eole The Frenchman Clement Ader constructed his first of three flying machines in 1886 the Eole It was a bat like design run by a lightweight steam engine of his own invention with four cylinders developing 20 horsepower 15 kW driving a four blade propeller The engine weighed no more than 4 kilograms per kilowatt 6 6 lb hp The wings had a span of 14 m 46 ft All up weight was 300 kilograms 660 lb On 9 October 1890 Ader attempted to fly the Eole Aviation historians give credit to this effort as a powered take off and uncontrolled hop of approximately 50 m 160 ft at a height of approximately 200 mm 7 9 in 27 28 Ader s two subsequent machines were not documented to have achieved flight 29 The American Wright brothers flights in 1903 are recognized by the Federation Aeronautique Internationale FAI the standard setting and record keeping body for aeronautics as the first sustained and controlled heavier than air powered flight 4 By 1905 the Wright Flyer III was capable of fully controllable stable flight for substantial periods The Wright brothers credited Otto Lilienthal as a major inspiration for their decision to pursue manned flight Santos Dumont 14 bis between 1906 and 1907 In 1906 the Brazilian Alberto Santos Dumont made what was claimed to be the first airplane flight unassisted by catapult 30 and set the first world record recognized by the Aero Club de France by flying 220 meters 720 ft in less than 22 seconds 31 This flight was also certified by the FAI 32 33 An early aircraft design that brought together the modern monoplane tractor configuration was the Bleriot VIII design of 1908 It had movable tail surfaces controlling both yaw and pitch a form of roll control supplied either by wing warping or by ailerons and controlled by its pilot with a joystick and rudder bar It was an important predecessor of his later Bleriot XI Channel crossing aircraft of the summer of 1909 34 World War I served as a testbed for the use of the airplane as a weapon Airplanes demonstrated their potential as mobile observation platforms then proved themselves to be machines of war capable of causing casualties to the enemy The earliest known aerial victory with a synchronized machine gun armed fighter aircraft occurred in 1915 by German Luftstreitkrafte Leutnant Kurt Wintgens Fighter aces appeared the greatest by number of Aerial Combat victories was Manfred von Richthofen Following WWI aircraft technology continued to develop Alcock and Brown crossed the Atlantic non stop for the first time in 1919 The first international commercial flights took place between the United States and Canada in 1919 35 Airplanes had a presence in all the major battles of World War II They were an essential component of the military strategies of the period such as the German Blitzkrieg The Battle of Britain and the American and Japanese aircraft carrier campaigns of the Pacific War Development of jet aircraft The Concorde supersonic transport aircraftThe first practical jet aircraft was the German Heinkel He 178 which was tested in 1939 In 1943 the Messerschmitt Me 262 the first operational jet fighter aircraft went into service in the German Luftwaffe The first jet airliner the de Havilland Comet was introduced in 1952 The Boeing 707 the first widely successful commercial jet was in commercial service for more than 50 years from 1958 to 2010 The Boeing 747 was the world s biggest passenger aircraft from 1970 until it was surpassed by the Airbus A380 in 2005 Supersonic airliner flights including those of the Concorde have been limited to over water flight at supersonic speed because of their sonic boom which is prohibited over most populated land areas The high cost of operation per passenger mile and a deadly crash in 2000 induced the operators of the Concorde to remove it from service 36 37 PropulsionSee also Powered aircraft and Aircraft engine Propeller Main articles Propeller aeronautics and Aircraft engine An Antonov An 2 biplane An aircraft propeller or airscrew converts rotary motion from an engine or other power source into a swirling slipstream which pushes the propeller forwards or backwards It comprises a rotating power driven hub to which are attached two or more radial airfoil section blades such that the whole assembly rotates about a longitudinal axis 38 Three types of aviation engines used to power propellers include reciprocating engines or piston engines gas turbines and electric motors The amount of thrust a propeller creates is determined in part by its disk area the area through which the blades rotate The limitation on blade speed is the speed of sound as when the blade tip exceeds the speed of sound shock waves decrease propeller efficiency The rpm required to generate a given tip speed is inversely proportional to the diameter of the propeller The upper design speed limit for propeller driven aircraft is Mach 0 6 Aircraft designed to go faster than that employ jet engines 39 Reciprocating engine Main articles Radial engine Inline engine aeronautics and Flat engine Reciprocating engines in aircraft have three main variants radial in line and flat or horizontally opposed engine The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders radiate outward from a central crankcase like the spokes of a wheel and was commonly used for aircraft engines before gas turbine engines became predominant An inline engine is a reciprocating engine with banks of cylinders one behind another rather than rows of cylinders with each bank having any number of cylinders but rarely more than six and may be water cooled A flat engine is an internal combustion engine with horizontally opposed cylinders Gas turbine Main article Turboprop A turboprop gas turbine engine consists of an intake compressor combustor turbine and a propelling nozzle which provide power from a shaft through a reduction gearing to the propeller The propelling nozzle provides a relatively small proportion of the thrust generated by a turboprop Electric motor Solar Impulse 1 a solar powered aircraft with electric motors Main article Electric motor An electric aircraft runs on electric motors with electricity coming from fuel cells solar cells ultracapacitors power beaming 40 or batteries Currently flying electric aircraft are mostly experimental prototypes including manned and unmanned aerial vehicles but there are some production models on the market 41 Jet Main article Jet engineJet aircraft are propelled by jet engines which are used because the aerodynamic limitations of propellers do not apply to jet propulsion These engines are much more powerful than a reciprocating engine for a given size or weight and are comparatively quiet and work well at higher altitude Variants of the jet engine include the ramjet and the scramjet which rely on high airspeed and intake geometry to compress the combustion air prior to the introduction and ignition of fuel Rocket motors provide thrust by burning a fuel with an oxidizer and expelling gas through a nozzle Turbofan Most jet aircraft use turbofan jet engines which employ a gas turbine to drive a ducted fan which accelerates air around the turbine to provide thrust in addition to that which is accelerated through the turbine The ratio of air passing around the turbine to that passing through is called the by pass ratio 42 They represent a compromise between turbojet with no bypass and turboprop forms of aircraft propulsion primarily powered with bypass air 43 Subsonic aircraft such as airliners employ high by pass jet engines for fuel efficiency Supersonic aircraft such as jet fighters use low bypass turbofans However at supersonic speeds the air entering the engine must be decelerated to a subsonic speed and then re accelerated back to supersonic speeds after combustion An afterburner may be used on combat aircraft to increase power for short periods of time by injecting fuel directly into the hot exhaust gases Many jet aircraft also use thrust reversers to slow down after landing 43 Ramjet Main article Ramjet Artist s concept of X 43A with scramjet attached to the underside A ramjet is a form of jet engine that contains no major moving parts and can be particularly useful in applications requiring a small and simple engine for high speed use such as with missiles Ramjets require forward motion before they can generate thrust and so are often used in conjunction with other forms of propulsion or with an external means of achieving sufficient speed The Lockheed D 21 was a Mach 3 ramjet powered reconnaissance drone that was launched from a parent aircraft A ramjet uses the vehicle s forward motion to force air through the engine without resorting to turbines or vanes Fuel is added and ignited which heats and expands the air to provide thrust 44 Scramjet Main article Scramjet A scramjet is a specialized ramjet that uses internal supersonic airflow to compress combine with fuel combust and accelerate the exhaust to provide thrust The engine operates at supersonic speeds only The NASA X 43 an experimental unmanned scramjet set a world speed record in 2004 for a jet powered aircraft with a speed of Mach 9 7 nearly 12 100 kilometers per hour 7 500 mph 45 Rocket Main article Rocket engine Bell X 1 in flight 1947 Whereas jet aircraft use the atmosphere both as a source of oxidant and of mass to accelerate reactively behind the aircraft rocket aircraft carry the oxidizer on board and accelerate the burned fuel and oxidizer backwards as the sole source of mass for reaction Liquid fuel and oxidizer may be pumped into a combustion chamber or a solid fuel with oxidizer may burn in the fuel chamber Whether liquid or solid fueled the hot gas is accelerated through a nozzle 46 In World War II the Germans deployed the Me 163 Komet rocket powered aircraft The first plane to break the sound barrier in level flight was a rocket plane the Bell X 1 in 1948 The North American X 15 broke many speed and altitude records in the 1960s and pioneered engineering concepts for later aircraft and spacecraft Military transport aircraft may employ rocket assisted take offs for short field situations Otherwise rocket aircraft include spaceplanes like SpaceShipTwo for travel beyond the Earth s atmosphere and sport aircraft developed for the short lived Rocket Racing League Design and manufactureMain article Aerospace manufacturer Assembly line of the SR 71 Blackbird at Skunk Works Lockheed Martin s Advanced Development Programs ADP Most airplanes are constructed by companies with the objective of producing them in quantity for customers The design and planning process including safety tests can last up to four years for small turboprops or longer for larger planes During this process the objectives and design specifications of the aircraft are established First the construction company uses drawings and equations simulations wind tunnel tests and experience to predict the behavior of the aircraft Computers are used by companies to draw plan and do initial simulations of the aircraft Small models and mockups of all or certain parts of the plane are then tested in wind tunnels to verify its aerodynamics When the design has passed through these processes the company constructs a limited number of prototypes for testing on the ground Representatives from an aviation governing agency often make a first flight The flight tests continue until the aircraft has fulfilled all the requirements Then the governing public agency of aviation of the country authorizes the company to begin production In the United States this agency is the Federal Aviation Administration FAA In the European Union European Aviation Safety Agency EASA in the United Kingdom it is the Civil Aviation Authority CAA 47 In Canada the public agency in charge and authorizing the mass production of aircraft is Transport Canada s Civil Aviation Authority 48 When a part or component needs to be joined together by welding for virtually any aerospace or defense application it must meet the most stringent and specific safety regulations and standards Nadcap or the National Aerospace and Defense Contractors Accreditation Program sets global requirements for quality quality management and quality assurance for aerospace engineering 49 In the case of international sales a license from the public agency of aviation or transport of the country where the aircraft is to be used is also necessary For example airplanes made by the European company Airbus need to be certified by the FAA to be flown in the United States and airplanes made by U S based Boeing need to be approved by the EASA to be flown in the European Union 50 An Airbus A321 on final assembly line 3 in the Airbus Hamburg Finkenwerder plant Regulations have resulted in reduced noise from aircraft engines in response to increased noise pollution from growth in air traffic over urban areas near airports 51 Small planes can be designed and constructed by amateurs as homebuilts Other homebuilt aircraft can be assembled using pre manufactured kits of parts that can be assembled into a basic plane and must then be completed by the builder 52 Few companies produce planes on a large scale However the production of a plane for one company is a process that actually involves dozens or even hundreds of other companies and plants that produce the parts that go into the plane For example one company can be responsible for the production of the landing gear while another one is responsible for the radar The production of such parts is not limited to the same city or country in the case of large plane manufacturing companies such parts can come from all over the world citation needed The parts are sent to the main plant of the plane company where the production line is located In the case of large planes production lines dedicated to the assembly of certain parts of the plane can exist especially the wings and the fuselage citation needed When complete a plane is rigorously inspected to search for imperfections and defects After approval by inspectors the plane is put through a series of flight tests to assure that all systems are working correctly and that the plane handles properly Upon passing these tests the plane is ready to receive the final touchups internal configuration painting etc and is then ready for the customer citation needed Characteristics Major components of an airplane An IAI Heron an unmanned aerial vehicle with a twin boom configuration Airframe Main article Airframe The structural parts of a fixed wing aircraft are called the airframe The parts present can vary according to the aircraft s type and purpose Early types were usually made of wood with fabric wing surfaces When engines became available for powered flight around a hundred years ago their mounts were made of metal Then as speeds increased more and more parts became metal until by the end of WWII all metal aircraft were common In modern times increasing use of composite materials has been made Typical structural parts include One or more large horizontal wings often with an airfoil cross section shape The wing deflects air downward as the aircraft moves forward generating lifting force to support it in flight The wing also provides stability in roll to stop the aircraft from rolling to the left or right in steady flight The An 225 Mriya which could carry a 250 tonne payload had two vertical stabilizers A fuselage a long thin body usually with tapered or rounded ends to make its shape aerodynamically smooth The fuselage joins the other parts of the airframe and usually contains important things such as the pilot payload and flight systems A vertical stabilizer or fin is a vertical wing like surface mounted at the rear of the plane and typically protruding above it The fin stabilizes the plane s yaw turn left or right and mounts the rudder which controls its rotation along that axis A horizontal stabilizer or tailplane usually mounted at the tail near the vertical stabilizer The horizontal stabilizer is used to stabilize the plane s pitch tilt up or down and mounts the elevators which provide pitch control Landing gear a set of wheels skids or floats that support the plane while it is on the surface On seaplanes the bottom of the fuselage or floats pontoons support it while on the water On some planes the landing gear retracts during flight to reduce drag Wings Main article Wing The wings of a fixed wing aircraft are static planes extending either side of the aircraft When the aircraft travels forwards air flows over the wings which are shaped to create lift This shape is called an airfoil and is shaped like a bird s wing Wing structure Airplanes have flexible wing surfaces which are stretched across a frame and made rigid by the lift forces exerted by the airflow over them Larger aircraft have rigid wing surfaces which provide additional strength Whether flexible or rigid most wings have a strong frame to give them their shape and to transfer lift from the wing surface to the rest of the aircraft The main structural elements are one or more spars running from root to tip and many ribs running from the leading front to the trailing rear edge Early airplane engines had little power and lightness was very important Also early airfoil sections were very thin and could not have a strong frame installed within So until the 1930s most wings were too lightweight to have enough strength and external bracing struts and wires were added When the available engine power increased during the 1920s and 30s wings could be made heavy and strong enough that bracing was not needed any more This type of unbraced wing is called a cantilever wing Wing configuration Main article Wing configuration Captured Morane Saulnier L wire braced parasol monoplane The number and shape of the wings varies widely on different types A given wing plane may be full span or divided by a central fuselage into port left and starboard right wings Occasionally even more wings have been used with the three winged triplane achieving some fame in WWI The four winged quadruplane and other multiplane designs have had little success A monoplane has a single wing plane a biplane has two stacked one above the other a tandem wing has two placed one behind the other When the available engine power increased during the 1920s and 30s and bracing was no longer needed the unbraced or cantilever monoplane became the most common form of powered type The wing planform is the shape when seen from above To be aerodynamically efficient a wing should be straight with a long span from side to side but have a short chord high aspect ratio But to be structurally efficient and hence light weight a wing must have a short span but still enough area to provide lift low aspect ratio At transonic speeds near the speed of sound it helps to sweep the wing backwards or forwards to reduce drag from supersonic shock waves as they begin to form The swept wing is just a straight wing swept backwards or forwards Two Dassault Mirage G prototypes one with wings swept The delta wing is a triangle shape that may be used for several reasons As a flexible Rogallo wing it allows a stable shape under aerodynamic forces and so is often used for ultralight aircraft and even kites As a supersonic wing it combines high strength with low drag and so is often used for fast jets A variable geometry wing can be changed in flight to a different shape The variable sweep wing transforms between an efficient straight configuration for takeoff and landing to a low drag swept configuration for high speed flight Other forms of variable planform have been flown but none have gone beyond the research stage Fuselage Main article Fuselage A fuselage is a long thin body usually with tapered or rounded ends to make its shape aerodynamically smooth The fuselage may contain the flight crew passengers cargo or payload fuel and engines The pilots of manned aircraft operate them from a cockpit located at the front or top of the fuselage and equipped with controls and usually windows and instruments A plane may have more than one fuselage or it may be fitted with booms with the tail located between the booms to allow the extreme rear of the fuselage to be useful for a variety of purposes Wings vs bodies Flying wing Main article Flying wing The US produced B 2 Spirit is a strategic bomber It has a flying wing configuration and is capable of intercontinental missions A flying wing is a tailless aircraft which has no definite fuselage Most of the crew payload and equipment are housed inside the main wing structure 53 The flying wing configuration was studied extensively in the 1930s and 1940s notably by Jack Northrop and Cheston L Eshelman in the United States and Alexander Lippisch and the Horten brothers in Germany After the war several experimental designs were based on the flying wing concept but the known difficulties remained intractable Some general interest continued until the early 1950s but designs did not necessarily offer a great advantage in range and presented several technical problems leading to the adoption of conventional solutions like the Convair B 36 and the B 52 Stratofortress Due to the practical need for a deep wing the flying wing concept is most practical for designs in the slow to medium speed range and there has been continual interest in using it as a tactical airlifter design Interest in flying wings was renewed in the 1980s due to their potentially low radar reflection cross sections Stealth technology relies on shapes which only reflect radar waves in certain directions thus making the aircraft hard to detect unless the radar receiver is at a specific position relative to the aircraft a position that changes continuously as the aircraft moves This approach eventually led to the Northrop B 2 Spirit stealth bomber In this case the aerodynamic advantages of the flying wing are not the primary needs However modern computer controlled fly by wire systems allowed for many of the aerodynamic drawbacks of the flying wing to be minimized making for an efficient and stable long range bomber Blended wing body Main article Blended wing Computer generated model of the Boeing X 48 Blended wing body aircraft have a flattened and airfoil shaped body which produces most of the lift to keep itself aloft and distinct and separate wing structures though the wings are smoothly blended in with the body Thus blended wing bodied aircraft incorporate design features from both a futuristic fuselage and flying wing design The purported advantages of the blended wing body approach are efficient high lift wings and a wide airfoil shaped body This enables the entire craft to contribute to lift generation with the result of potentially increased fuel economy Lifting body The Martin Aircraft Company X 24 was built as part of a 1963 to 1975 experimental US military program Main article Lifting body A lifting body is a configuration in which the body itself produces lift In contrast to a flying wing which is a wing with minimal or no conventional fuselage a lifting body can be thought of as a fuselage with little or no conventional wing Whereas a flying wing seeks to maximize cruise efficiency at subsonic speeds by eliminating non lifting surfaces lifting bodies generally minimize the drag and structure of a wing for subsonic supersonic and hypersonic flight or spacecraft re entry All of these flight regimes pose challenges for proper flight stability Lifting bodies were a major area of research in the 1960s and 70s as a means to build a small and lightweight manned spacecraft The US built several famous lifting body rocket planes to test the concept as well as several rocket launched re entry vehicles that were tested over the Pacific Interest waned as the US Air Force lost interest in the manned mission and major development ended during the Space Shuttle design process when it became clear that the highly shaped fuselages made it difficult to fit fuel tankage Empennage and foreplane Main articles Empennage and Canard aeronautics Canards on the Saab Viggen The classic airfoil section wing is unstable in flight and difficult to control Flexible wing types often rely on an anchor line or the weight of a pilot hanging beneath to maintain the correct attitude Some free flying types use an adapted airfoil that is stable or other ingenious mechanisms including most recently electronic artificial stability To achieve stability and control most fixed wing types have an empennage comprising a fin and rudder which act horizontally and a tailplane and elevator which act vertically These control surfaces can typically be trimmed to relieve control forces for various stages of flight This is so common that it is known as the conventional layout Sometimes there may be two or more fins spaced out along the tailplane Some types have a horizontal canard foreplane ahead of the main wing instead of behind it 54 55 56 This foreplane may contribute to the lift the trim or control of the aircraft or to several of these Controls and instruments Main article Aircraft flight control system A light aircraft Robin DR400 500 cockpit Further information Fixed wing aircraft Aircraft controls and Fixed wing aircraft Cockpit instrumentation Airplanes have complex flight control systems The main controls allow the pilot to direct the aircraft in the air by controlling the attitude roll pitch and yaw and engine thrust On manned aircraft cockpit instruments provide information to the pilots including flight data engine output navigation communications and other aircraft systems that may be installed SafetyMain article Aviation safety When risk is measured by deaths per passenger kilometer air travel is approximately 10 times safer than travel by bus or rail However when using the deaths per journey statistic air travel is significantly more dangerous than car rail or bus travel 57 Air travel insurance is relatively expensive for this reason insurers generally use the deaths per journey statistic 58 There is a significant difference between the safety of airliners and that of smaller private planes with the per mile statistic indicating that airliners are 8 3 times safer than smaller planes 59 Environmental impactMain article Environmental impact of aviation Water vapor contrails left by high altitude jet airliners These may contribute to cirrus cloud formation Like all activities involving combustion fossil fuel powered aircraft release soot and other pollutants into the atmosphere Greenhouse gases such as carbon dioxide CO2 are also produced In addition there are environmental impacts specific to airplanes for instance Airplanes operating at high altitudes near the tropopause mainly large jet airliners emit aerosols and leave contrails both of which can increase cirrus cloud formation cloud cover may have increased by up to 0 2 since the birth of aviation 60 Airplanes operating at high altitudes near the tropopause can also release chemicals that interact with greenhouse gases at those altitudes particularly nitrogen compounds which interact with ozone increasing ozone concentrations 61 62 Most light piston aircraft burn avgas which contains tetraethyllead TEL Some lower compression piston engines can operate on unleaded mogas and turbine engines and diesel engines neither of which require lead are used on some newer light aircraft Some non polluting light electric aircraft are already in production Another environmental impact of airplanes is noise pollution mainly caused by aircraft taking off and landing See also Aviation portalAircraft flight mechanics Aviation Fuel efficiency List of altitude records reached by different aircraft types RotorcraftReferences Global air traffic hits new record Channel News Asia 18 January 2018 Archived from the original on 3 January 2021 Retrieved 28 May 2022 Measured in RTKs an RTK is one tonne of revenue freight carried one kilometer Crabtree Tom Hoang Tom Tom Russell 2016 World Air Cargo Forecast 2016 2017 PDF Boeing Aircraft Retrieved 12 May 2018 a b FAI News 100 Years Ago the Dream of Icarus Became Reality Archived January 13 2011 at the Wayback Machine posted 17 December 2003 Retrieved 5 January 2007 a b Cayley Sir George Encyclopaedia Britannica 2007 Encyclopaedia Britannica Online 25 August 2007 Otto Lilienthal Museum Otto Lilienthal Museum Anklam Lilienthal museum de Retrieved 4 March 2022 ἀhr Henry George Liddell Robert Scott A Greek English Lexicon on Perseus aeroplane Merriam Webster Online Dictionary planos Henry George Liddell Robert Scott A Greek English Lexicon on Perseus aeroplane Oxford Dictionaries a b aeroplane Oxford English Dictionary online Aulus Gellius Attic Nights Book X 12 9 at LacusCurtius Archytas of Tarentum Technology Museum of Thessaloniki Macedonia Greece Tmth edu gr Archived from the original on 26 December 2008 Retrieved 30 May 2013 Modern rocketry Pressconnects com Retrieved 30 May 2013 permanent dead link Automata history Automata co uk Archived from the original on 5 December 2002 Retrieved 30 May 2013 White Lynn Eilmer of Malmesbury an Eleventh Century Aviator A Case Study of Technological Innovation Its Context and Tradition Technology and Culture Volume 2 Issue 2 1961 pp 97 111 97 99 resp 100 101 Aviation History Retrieved 26 July 2009 In 1799 he set forth for the first time in history the concept of the modern aeroplane Cayley had identified the drag vector parallel to the flow and the lift vector perpendicular to the flow Sir George Cayley British Inventor and Scientist Britannica Retrieved 26 July 2009 English pioneer of aerial navigation and aeronautical engineering and designer of the first successful glider to carry a human being aloft Cayley established the modern configuration of an airplane as a fixed wing flying machine with separate systems for lift propulsion and control as early as 1799 E Hendrickson III Kenneth The Encyclopedia of the Industrial Revolution in World History Volume 3 p 10 The Journal of San Diego History July 1968 Vol 14 No 3 Beril Becker 1967 Dreams and Realities of the Conquest of the Skies New York Atheneum pp 124 125 Inglis Amirah Hargrave Lawrence 1850 1915 Australian Dictionary of Biography Vol 9 Melbourne University Press Retrieved 5 July 2010 Otto Lilienthal Museum Otto Lilienthal Museum Anklam Lilienthal museum de Retrieved 4 March 2022 The Lilienthal glider project DLR Portal Dlr de Retrieved 4 March 2022 Otto Lilienthal Museum Otto Lilienthal Museum Anklam Lilienthal museum de Retrieved 4 March 2022 Crouch 1989 pp 226 228 Gibbs Smith Charles H 3 April 1959 Hops and Flights A roll call of early powered take offs Flight 75 2619 468 Archived from the original on 2 March 2012 Retrieved 24 August 2013 European Aeronautic Defence and Space Company EADS N V Eole Clement Ader Archived from the original on 20 October 2007 Retrieved 20 October 2007 Gibbs Smith Charles Harvard 1968 Clement Ader His Flight Claims and His Place in History Aeronautical engineers London Her Majesty s Stationery Office p 214 Bernardo Malfitano AirShowFan com airshowfan com Archived from the original on 30 March 2013 Retrieved 1 April 2015 Jones Ernest Santos Dumont in France 1906 1916 The Very Earliest Early Birds Archived 2016 03 16 at the Wayback Machine earlyaviators com 25 December 2006 Retrieved 17 August 2009 Les vols du 14bis relates au fil des editions du journal l illustration de 1906 The wording is cette prouesse est le premier vol au monde homologue par l Aero Club de France et la toute jeune Federation Aeronautique Internationale FAI Santos Dumont Pionnier de l aviation dandy de la Belle Epoque Crouch Tom 1982 Bleriot XI The Story of a Classic Aircraft Smithsonian Institution Press pp 21 and 22 ISBN 0 87474 345 1 C Brunco Leonard 1993 On the Move A Chronology of Advances in Transportation Gale Research p 192 Concorde grounded for good 10 April 2003 Retrieved 18 December 2021 Filseth Trevor 4 December 2021 Why Don t Concordes Fly Anymore The National Interest Retrieved 18 December 2021 Beaumont R A Aeronautical Engineering Odhams 1942 Chapter 13 Airscrews Sadraey Mohammad H 1 January 2017 Aircraft Performance An Engineering Approach CRC Press p 137 ISBN 9781498776561 Power Beaming Archived 2013 02 17 at the Wayback Machine Dfrc nasa gov Pipistrel Expands Electric Aircraft Line 2013 Cumpsty Nicholas Heyes Andrew 22 July 2015 Jet Propulsion A Simple Guide to the Aerodynamics and Thermodynamic Design and Performance of Jet Engines Cambridge University Press ISBN 978 1 316 43263 1 a b El Sayed Ahmed F 6 July 2017 Aircraft Propulsion and Gas Turbine Engines CRC Press pp 43 770 ISBN 978 1 4665 9517 0 Here Comes the Flying Stovepipe Time 26 November 1965 Archived from the original on 8 April 2008 Retrieved 8 April 2008 Weber Richard J Mackay John S September 1958 An Analysis of Ramjet Engines Using Supersonic Combustion ntrs nasa gov NASA Scientific and Technical Information Retrieved 3 May 2016 Sutton George P Biblarz Oscar 27 December 2016 Rocket Propulsion Elements John Wiley amp Sons p 29 ISBN 978 1 118 75365 1 UK will leave EU aviation safety regulator at end of 2020 BBC News 7 March 2020 Retrieved 19 December 2021 Canada Transport 15 October 2019 Civil Aviation Transport Canada Retrieved 19 December 2021 Aerospace Welding Helander Metal Helander Metal Retrieved 27 December 2017 Our Mission Your Safety EASA 2021 Archived from the original on 11 June 2020 Retrieved 19 December 2021 Reducing noise aviationbenefits org Retrieved 15 April 2021 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Global Atmosphere Bibcode 1999aga book P Archived from the original on 29 June 2007 Lin X Trainer M amp Liu S C 1988 On the nonlinearity of the tropospheric ozone production Journal of Geophysical Research 93 D12 15879 15888 Bibcode 1988JGR 9315879L doi 10 1029 JD093iD12p15879 Grewe V D Brunner M Dameris J L Grenfell R Hein D Shindell J Staehelin July 2001 Origin and variability of upper tropospheric nitrogen oxides and ozone at northern mid latitudes Atmospheric Environment 35 20 3421 33 Bibcode 2001AtmEn 35 3421G doi 10 1016 S1352 2310 01 00134 0 hdl 2060 20000060827 BibliographyBlatner David The Flying Book Everything You ve Ever Wondered About Flying On Airplanes ISBN 0 8027 7691 4External links Wikiquote has quotations related to Airplane Look up aeroplane aircraft or airplane in Wiktionary the free dictionary The Aeroplane centre Airliners net Aerospaceweb org How Airplanes Work Howstuffworks com Retrieved from https en wikipedia org w index php title Airplane amp oldid 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