Case of small single seater only examined; requirements are high speed, high ceiling and quick rate of climb, good maneuverability, powerful armament, small size, slow landing speed, and as long range as practicable; aerodynamic cleanliness; aspect ratio: propeller design; cooling system; intakes and exhausts; choice of airfoil section; stability and control; structural problems.
Fundamentals of fighter design
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 46 , n 383
1942
20 pages
Article (Journal)
English
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