Constructional features and production methods described and illustrated; all metal stressed skin construction; engine submerged amidships, tricycle undercarriage; engine is 12-cyl liquid cooled Allison V 1710 which develops 1325 hp at take-off; wing span 34 ft; oa length 34 ft 2 in.; oa height 9 ft 3 in.; wing area 213 sq ft. (See also Aircraft Production v 3 n 36 Oct 1941 p 364-7; Aeroplane v 61 n 1587 and 1588 Oct 24 1941 p 448-9 and Oct 31 p 476-9)
Originality in bell airacobra
Automotive Industries
Automotive Industries ; 85 , n 12
1941
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
TIBKAT | 1967
|Fahrwerk des Beuteflugzeuges Bell Airacobra (P 39)
SLUB | 1942
|Aerodynamics of the Bell P-39 Airacobra and P-63 Kingcobra
SAE Technical Papers | 2000
|Aerodynamics of the Bell P-39 Airacobra and P-63 Kingcobra
British Library Conference Proceedings | 2000
|