In aerodynamics, climb gradient is the ratio between distance travelled over the ground and altitude gained, and is expressed as a percentage. The angle of climb can be defined as the angle between a horizontal plane representing the Earth's surface and the actual flight path followed by the aircraft during its ascent.
Best Angle of Climb for a jet and a propeller aircraftBest Angle of Climb as a function of altitude
The speed of an aircraft type at which the angle of climb is largest is called VX. It is always slower than VY, the speed for the best rate of climb. As the latter gives the quickest way for gaining altitude levels, regardless of the distance covered during such a maneuver, it is more relevant to cruising. The maximum angle of climb on the other hand is where the aircraft gains the most altitude in a given distance, regardless of the time needed for the maneuver. This is important for clearing an obstacle, and therefore is the speed a pilot uses when executing a "short field" takeoff. VX increases with altitude and VY decreases with altitude until they converge at the airplane's absolute ceiling.
Best angle of climb (BAOC) airspeed for an airplane is the speed at which the maximum excess thrust is available. Excess thrust is the difference between the total drag of the aircraft, and the thrust output of the powerplant. For a jet aircraft, this speed is very close to the speed at which the total minimum drag occurs.
angle, climb, this, article, does, cite, sources, please, help, improve, this, article, adding, citations, reliable, sources, unsourced, material, challenged, removed, find, sources, news, newspapers, books, scholar, jstor, 2021, learn, when, remove, this, mes. This article does not cite any sources Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources Angle of climb news newspapers books scholar JSTOR May 2021 Learn how and when to remove this message In aerodynamics climb gradient is the ratio between distance travelled over the ground and altitude gained and is expressed as a percentage The angle of climb can be defined as the angle between a horizontal plane representing the Earth s surface and the actual flight path followed by the aircraft during its ascent Best Angle of Climb for a jet and a propeller aircraft Best Angle of Climb as a function of altitude The speed of an aircraft type at which the angle of climb is largest is called VX It is always slower than VY the speed for the best rate of climb As the latter gives the quickest way for gaining altitude levels regardless of the distance covered during such a maneuver it is more relevant to cruising The maximum angle of climb on the other hand is where the aircraft gains the most altitude in a given distance regardless of the time needed for the maneuver This is important for clearing an obstacle and therefore is the speed a pilot uses when executing a short field takeoff VX increases with altitude and VY decreases with altitude until they converge at the airplane s absolute ceiling Best angle of climb BAOC airspeed for an airplane is the speed at which the maximum excess thrust is available Excess thrust is the difference between the total drag of the aircraft and the thrust output of the powerplant For a jet aircraft this speed is very close to the speed at which the total minimum drag occurs See also editRate of climbReferences edit nbsp This fluid dynamics related article is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title Angle of climb amp oldid 1098865851, wikipedia, wiki, book, books, library,
