It is concluded that delta wing, contrary to widely publicized opinion that it is destined to be wing planform for all future supersonic aircraft, actually offers only limited range of Mach number usefulness, that between 1.0 and 1.4, but this is next important speed regime into which aircraft design is now moving; beyond this speed, however, straight wing is certain to be the answer.


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    Titel :

    Delta wing


    Weitere Titelangaben:

    Aero Digest


    Erschienen in:

    Aero Digest ; 61 , n 6


    Erscheinungsdatum :

    1950


    Format / Umfang :

    12 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Delta Wing Configurations

    J. Szodruch | NTIS | 1988


    Moulded Delta wing

    Engineering Index Backfile | 1951


    The pitching delta wing

    Gad-el-Hak, M. / Ho, C.M. | Tema Archiv | 1985


    Delta wing design analysis

    Schuerch, H.U. | Engineering Index Backfile | 1953


    The pitching delta wing

    GAD-EL-HAK, M. / HO, C.-M. | AIAA | 1985