A new two dimensional thrust augmenter VTOL model has been designed, built and tested. The model has few moving parts and possibilities for good aerodynamic performance. A complete static test facility capable of supplying 30 psig air through 1.5 square inches nozzle for 2 minutes has been built for testing this model. The test rig can be moved in and out of ground effect by a fork lift. Instrumentation consists of strain gages to measure total lift and thrust.


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    Titel :

    Inlet and Internal Aerodynamics of a VTOL Thrust Augmenter


    Beteiligte:
    J. L. Loth (Autor:in) / S. Chandra (Autor:in) / E. H. Gibbs (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    96 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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