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.


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    Title :

    Fundamentals of fighter design


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1942


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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