Armstrong Whitworth Starling

The Armstrong Whitworth A.W.14 Starling was a prototype British single-seat biplane fighter developed for the Royal Air Force in the late 1920s which unsuccessfully competed against the Bristol Bulldog.

Development

The A.W.14 Starling was developed by Armstrong Whitworth as the sole contender for Specification 28/24, for a single-seat fighter capable of operating in day and night-time conditions to replace Armstrong Whitworth's earlier Siskin. It was a single- bay sesquiplane (a biplane with the lower wing much smaller than the upper) with staggered unequal span wings. The fuselage had a bolted steel-tube structure, while the wings had steel spars and wooden ribs and were fitted with ailerons on the upper wings only. The wings used the experimental symmetrical RAF 30 aerofoil section. Armament was two synchronised Vickers machine guns.Tapper 1988, pp. 168–170.Mason 1992, p. 189.''Flight'' 2 August 1928, pp. 660–665.

Two prototypes were ordered, with the first ''J8027'', powered by a Armstrong Siddeley Jaguar VII radial engine which was flown on 12 May 1927. It was underpowered, and was re-engined with a Jaguar V engine but its performance remained unimpressive, with the first prototype failed to exceed , well short of the required , while low speed handling was also poor.Tapper 1988, p. 170. The prototype was evaluated against the later Specification F.9/26 in February 1926, but was rejected by the RAF, who instead selected the Bristol Bulldog. ''J8027'' was returned to Armstrong Whitworth, who fitted it with new wings with a Clark YH aerofoil section and leading edge slots on the upper wings.Tapper 1988, pp. 170–171. With the civil registration ''G-AAHC'' it was shown at Olympia in London in July 1929 and was cancelled from the register in December 1930.Jackson 1974, p. 323.

The second prototype, ''J8028'' was extensively redesigned, with a more streamlined fuselage and revised wings, which although retaining the Clark YH aerofoil section, had smaller lower wings.Tapper 1988, pp. 173, 175. Powered by a Armstrong Siddeley Panther II engine, it first flew on 5 December 1929. It was evaluated as both a land-based interceptor against Specifications F.9/26 and F.20/27Tapper 1988, p. 176.Williams ''Aeroplane Monthly'' July 1980, pp. 370–371. and as a naval fighter to meet the requirements of Specification N.21/26. Performance was improved but it was also unsuccessful, although it did carry out useful development work for the Armstrong Whitworth A.W.16.

Variants

;Starling I
:1927 – first prototype – powered by Armstrong Siddeley Jaguar VII or V engine.
;Starling II
:1930 – second prototype – specification N.21/26 for a naval fighter. Powered by Armstrong Siddeley Panther II engine.

Operators

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Specifications (Starling I)

See also

References

Citations

Bibliography

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External links

RAF 30 aerofoil section used on first prototypeClark YH aerofuil section used following modifications

{{Armstrong Whitworth aircraft

Sesquiplanes
Single-engined tractor aircraft
1920s British fighter aircraft
Starling
Aircraft first flown in 1927