Tunnel utilizing US Navy airship as stable model carriage developed by Subsonic Aerodynamics Laboratory of Princeton Univ is shown to give accurate, repeatable data for variety of configurations; details of ZS2G-1 used in initial feasibility studies, and ZPG-2 airship having increased endurance and capability; results with respect to velocity survey, vibration level, adaptability of mounting system, available power supply, ease of calibration, and access to model and ease of testing.


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    Title :

    Navy's flying wind tunnel


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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