Factors relating to power plant problem for high speed aircraft concentrating mainly on problem of wing planforms and overall aircraft configurations for Mach number range of 0 to 2; thin, straight wing best up to Mach 2; delta or swept designs do not match lift or handling features of straight wing. (see also Aviation Week n 23 Dec 7 1953 p 26, 28, 31, 33-4, 37)


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    Title :

    Airplane configurations for high speed flight


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1953 Design



    Publication date :

    1953


    Size :

    16 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1954


    Airplane Configurations for High-Speed Flight

    Johnson, Clarence L. | SAE Technical Papers | 1954


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1953


    Airplane flight testing for maximum speed

    Thomas, F.M. / Fairchild, H.W. | Engineering Index Backfile | 1933


    Airplane Flight Testing for Maximum Speed

    Thomas, F. M. / Fairchild, H. W. | SAE Technical Papers | 1933