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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    Title :

    The requirements for a new full scale subsonic wind tunnel


    Contributors:

    Publication date :

    1972-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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