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Merville SM.31

The Merville SM.31 is a French high performance glider with a laminar flow wing, first flown in 1960. Only one was built.

SM.31
Role High performance glider
National origin France
Manufacturer Helice G. Merville
Designer R. Cartier
First flight 11 January 1960
Number built 1
Developed from Merville S.30

Design and development edit

In the 1960s, André Merville was president of the Boulogne- based company Helice G. Merville, which had been the chief supplier of wooden propellers for French aircraft since the end of World War I. He sought to broaden the firm's product range by producing both light aircraft and gliders. The SM.31 high-performance sailplane was a development of their S.30 (sometimes written SM.30).[1]

It is a wood-framed aircraft, covered with a mixture of plywood and fabric. Its wing was built around a single spar with ply covering from the spar around the leading edge and fabric aft. The smooth ply skin covers just over half the chord, matching the approximate distance over which the ideal NACA airfoil 654421 maintains laminar flow; the rest is fabric-covered, though the covering of the plain ailerons is a ply and fabric mixture. In plan the wing has a rectangular centre section reaching out to about 60% of the span. Its square tipped outer sections have a swept leading edge, giving them a 6° sweep at quarter chord and a taper ratio of 65%. The ailerons are each in two parts, operating differentially and occupying about 63% of the span; the rest of the trailing edge is filled with lift-increasing Fowler flaps. There are Schempp-Hirth type air brakes on the inner section at 57% chord. The wings are shoulder mounted with a dihedral of 2.5°.[2]

The fuselage of the SM.31 is ply covered over wooden frames and stringers. In section it is ovoid, deep and narrow in the single-seat cockpit area ahead of the wings. Its single-piece, blown perspex canopy occupies most of this forward region. It has a rounded profile which curves upwards into the upper fuselage line just ahead of the wing and is side opening. Aft, the fuselage tapers slowly to the tail, where the straight tapered tailplane and elevators are mounted on top. The fin is faired into the fuselage at its root but elsewhere the vertical tail is straight tapered and flat topped. The rudder, hinged behind the elevator trailing edge and extending down to the keel, is not balanced. All the fixed tail surfaces are ply covered, with fabric covered control surfaces. The SM.31 lands on a semi-recessed, unsprung monowheel, fitted with brakes and assisted by a fixed skid which stretches from nose the under the wing trailing edge together with a tail bumper protecting the rudder.[1][2]

The SM.31's first flight was made on 11 January 1960.[2] The sole example still exists, though neither airworthy nor on display. Whether it is F-CCHN in the Ailes Ancienne collection in Toulouse or F-CBYK at the Musée Régional de l'Air at Angers is not certain; one is probably the SM.30 and the other the SM.31.[3][4]


Specifications edit

Data from The World's Sailplanes II (1963) p.84-5[2]

General characteristics

  • Crew: One
  • Length: 8.10 m (26 ft 7 in) [1]
  • Wingspan: 18.06 m (59 ft 3 in)
  • Height: 1.80 m (5 ft 11 in) over tail[1]
  • Wing area: 18.0 m2 (194 sq ft)
  • Aspect ratio: 18
  • Airfoil: NACA airfoil 654421 at root, 643618 at tip
  • Empty weight: 360 kg (794 lb) equipped
  • Max takeoff weight: 460 kg (1,014 lb)
  • Maximum wing loading: 25.5 kg/m2 (5.24 lb/sqft)

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn) placard, smooth air
  • Maximimum speed: 180 km/h (112 mph) placard, rough air
  • Aerotowing speed: 100 km/h (62 mph)
  • Winch launch speed: 100 km/h (62 mph)
  • g limits: +5/-2
  • Maximum glide ratio: maximum 32.5:1, at 98 km/h (61 mph) and a weight of 440 kg (970 lb)
  • Rate of sink: 0.78 m/s (154 ft/min) minimum, at 80 km/h (50 mph) and a weight of 440 kg (970 lb), with no flaps


References edit

  1. ^ a b c d Taylor, John W R (1964). Jane's All the World's Aircraft 1964-65. London: Sampson Low, Marston & Co. Ltd. pp. 47, 358.
  2. ^ a b c d Shenstone, B.S.; Wilkinson, K.G. (1963). The World's Sailplanes. Vol. II. Organisation Scientifique et Technique Internationale du Vol à Voile (OSTIV) and Schweizer Aero-Revue. pp. 84–5.
  3. ^ "Murville SM.31". Retrieved 14 March 2014.
  4. ^ Ogden, Bob (2009). Aviation Museums and Collections of Mainland Europe. Air Britain (Historians) Ltd. pp. 126, 147. ISBN 978 0 85130 418 2.

merville, french, high, performance, glider, with, laminar, flow, wing, first, flown, 1960, only, built, 31role, high, performance, glidernational, origin, francemanufacturer, helice, mervilledesigner, cartierfirst, flight, january, 1960number, built, 1develop. The Merville SM 31 is a French high performance glider with a laminar flow wing first flown in 1960 Only one was built SM 31Role High performance gliderNational origin FranceManufacturer Helice G MervilleDesigner R CartierFirst flight 11 January 1960Number built 1Developed from Merville S 30Design and development editIn the 1960s Andre Merville was president of the Boulogne based company Helice G Merville which had been the chief supplier of wooden propellers for French aircraft since the end of World War I He sought to broaden the firm s product range by producing both light aircraft and gliders The SM 31 high performance sailplane was a development of their S 30 sometimes written SM 30 1 It is a wood framed aircraft covered with a mixture of plywood and fabric Its wing was built around a single spar with ply covering from the spar around the leading edge and fabric aft The smooth ply skin covers just over half the chord matching the approximate distance over which the ideal NACA airfoil 654421 maintains laminar flow the rest is fabric covered though the covering of the plain ailerons is a ply and fabric mixture In plan the wing has a rectangular centre section reaching out to about 60 of the span Its square tipped outer sections have a swept leading edge giving them a 6 sweep at quarter chord and a taper ratio of 65 The ailerons are each in two parts operating differentially and occupying about 63 of the span the rest of the trailing edge is filled with lift increasing Fowler flaps There are Schempp Hirth type air brakes on the inner section at 57 chord The wings are shoulder mounted with a dihedral of 2 5 2 The fuselage of the SM 31 is ply covered over wooden frames and stringers In section it is ovoid deep and narrow in the single seat cockpit area ahead of the wings Its single piece blown perspex canopy occupies most of this forward region It has a rounded profile which curves upwards into the upper fuselage line just ahead of the wing and is side opening Aft the fuselage tapers slowly to the tail where the straight tapered tailplane and elevators are mounted on top The fin is faired into the fuselage at its root but elsewhere the vertical tail is straight tapered and flat topped The rudder hinged behind the elevator trailing edge and extending down to the keel is not balanced All the fixed tail surfaces are ply covered with fabric covered control surfaces The SM 31 lands on a semi recessed unsprung monowheel fitted with brakes and assisted by a fixed skid which stretches from nose the under the wing trailing edge together with a tail bumper protecting the rudder 1 2 The SM 31 s first flight was made on 11 January 1960 2 The sole example still exists though neither airworthy nor on display Whether it is F CCHN in the Ailes Ancienne collection in Toulouse or F CBYK at the Musee Regional de l Air at Angers is not certain one is probably the SM 30 and the other the SM 31 3 4 Specifications editData from The World s Sailplanes II 1963 p 84 5 2 General characteristicsCrew One Length 8 10 m 26 ft 7 in 1 Wingspan 18 06 m 59 ft 3 in Height 1 80 m 5 ft 11 in over tail 1 Wing area 18 0 m2 194 sq ft Aspect ratio 18 Airfoil NACA airfoil 654421 at root 643618 at tip Empty weight 360 kg 794 lb equipped Max takeoff weight 460 kg 1 014 lb Maximum wing loading 25 5 kg m2 5 24 lb sqft Performance Maximum speed 220 km h 140 mph 120 kn placard smooth air Maximimum speed 180 km h 112 mph placard rough air Aerotowing speed 100 km h 62 mph Winch launch speed 100 km h 62 mph g limits 5 2 Maximum glide ratio maximum 32 5 1 at 98 km h 61 mph and a weight of 440 kg 970 lb Rate of sink 0 78 m s 154 ft min minimum at 80 km h 50 mph and a weight of 440 kg 970 lb with no flapsReferences edit a b c d Taylor John W R 1964 Jane s All the World s Aircraft 1964 65 London Sampson Low Marston amp Co Ltd pp 47 358 a b c d Shenstone B S Wilkinson K G 1963 The World s Sailplanes Vol II Organisation Scientifique et Technique Internationale du Vol a Voile OSTIV and Schweizer Aero Revue pp 84 5 Murville SM 31 Retrieved 14 March 2014 Ogden Bob 2009 Aviation Museums and Collections of Mainland Europe Air Britain Historians Ltd pp 126 147 ISBN 978 0 85130 418 2 Retrieved from https en wikipedia org w index php title Merville SM 31 amp oldid 1124718982, wikipedia, wiki, book, books, library,

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