Requirements for V/STOL aircraft introduce unique structural problems created by propulsion modes requiring increased thrust during hover and their relative airframe locations; paper considers design philosophy for fan-in-wing configurations to obtain optimum structural design, acoustic environment problems, such as noise attention and acoustic fatigue; study of thermal problems, both internal and external, and their effect on structure; problem of debris damage due to propulsion environment at ground hover; importance of structural weight/cost effectiveness is shown for V/STO L aircraft.


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    Titel :

    V/STOL aircraft structural considerations


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Alvey, V.W. (Autor:in) / Fried, H. (Autor:in)

    Kongress:

    SAE Meeting ; 1966 VTOL-STOL



    Erscheinungsdatum :

    1966


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    V/STOL Aircraft Structural Considerations

    Fried, H. / Alvey, V. W. | SAE Technical Papers | 1966


    Airworthiness considerations for STOL aircraft

    Holzhauser, C. A. / Innis, R. C. / Quigley, H. C. | NTRS | 1970


    Airworthiness Considerations for STOL Aircraft

    C. A. Holzhauser / R. C. Innis / H. C. Quigley | NTIS | 1970


    Airworthiness considerations for STOL aircraft

    Innis, Robert C. / Holzhauser, Curt A. / Quigley, Hervey C. | TIBKAT | 1970


    Stability and control considerations for STOL AIRCRAFT.

    Anderson, S. B. / Innis, R. C. / Quigley, H. C. | NTRS | 1966