THIS paper discusses problems encountered in the Mach number range of 0 to 2 with aircraft having different wing planforms. The delta-wing type is compared to the unswept or straight thin wing.It is concluded that, with the solution to the structural problem having been obtained for the latter wing, the unswept type is superior to the delta type when strictly comparative missions and operating field lengths are considered.THIS paper discusses problems encountered in the Mach number range of 0 to 2 with aircraft having different wing planforms. The delta-wing type is compared to the unswept or straight thin wing.It is concluded that, with the solution to the structural problem having been obtained for the latter wing, the unswept type is superior to the delta type when strictly comparative missions and operating field lengths are considered.


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    Titel :

    Airplane Configurations for High-Speed Flight


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1954-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Airplane configurations for high speed flight

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


    Airplane configurations for high speed flight

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


    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