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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    Titel :

    Navy's flying wind tunnel


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Payne, H.E. (Autor:in) / Carter III, F.R. (Autor:in) / Harrison, W.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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