Justification and requirements are presented for a large subsonic wind tunnel capable of testing full scale aircraft, rotor systems, and advanced V/STOL propulsion systems. The design considerations and constraints for such a facility are reviewed, and the trades between facility test capability and costs are discussed.


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    Titel :

    The requirements for a new full scale subsonic wind tunnel


    Beteiligte:
    Kelly, M. W. (Autor:in) / Mckinney, M. O. (Autor:in) / Luidens, R. W. (Autor:in)

    Erscheinungsdatum :

    01.02.1972


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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