A smooth variable camber wing system using flexible skins has been designed for fighter and attack airplanes. Comparisons of this system with other systems such as leading edge slats, plain flaps, canards and the box wing illustrate its overall performance superiority. Estimates of the performance improvements which result when smooth curved variable camber flaps are applied to the F-8, F-4, A-7, F-14, and S-3 show that any of these aircraft could benefit from the addition of this system. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Additional Studies, Variable Camber Wing - Phase I


    Beteiligte:
    D. K. Gould (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    47 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Loads Report Variable Camber Wing - Phase I

    P. Milns / A. F. Grisham | NTIS | 1973


    VARIABLE WING LEADING EDGE CAMBER

    PIPERNI PASQUALE | Europäisches Patentamt | 2023

    Freier Zugriff