Requirements of VTOL propulsion system lead to use of straight air intake configurations in which direction of intake axis can differ widely from direction of aircraft motion; data relating to mean total pressure loss and flow distortion in circular intakes under cross-flow conditions are presented for five cowl shapes; boundaries were established between regime in which cross-flow effects are small and regime characterized by flow separation; in latter, pressure loss and flow distortion are severe and dependent on cross-flow conditions.


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    Titel :

    Pressure loss and flow distortion measurements on circular compressor intakes in inclined flow


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    Tyler, R.A. (Autor:in) / Williamson, R.G. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




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