Existing criteria reflected in military specifications and standards and design guides are inadequate for V/STOL aircraft. The present criteria for helicopter design and testing are those which evolved and have been used over several years for U. S. Air Force fixed-wing aircraft. The helicopter takeoff and landing environment, particularly airborne particle concentration, is markedly more severe than that for fixed-wing aircraft. This report presents data and conclusions which can be used to establish design and testing criteria for future V/STOL aircraft. (Author)


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    Titel :

    Studies of the Army Aviation(V/STOL) Environment. Report No. 2. Particulate Matter Considerations in the Design of V/STOL Aircraft


    Beteiligte:
    J. Viletto (Autor:in) / H. L. Ohman (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    V/STOL aircraft structural considerations

    Alvey, V.W. / Fried, H. | Engineering Index Backfile | 1966


    Airworthiness Considerations for STOL Aircraft

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


    V/STOL Aircraft Structural Considerations

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


    Airworthiness considerations for STOL aircraft

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


    Airworthiness considerations for STOL aircraft

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