A study of several typical air inductions systems for modern aircraft indicate that flow distortions of about-pipe-flow magnitudes can be expected at near-optimum inlet-engine matched air-flow conditions and at small angles of attacks. These distortions may be seriously increased by operation at large angles of attack or yaw, or by supercritical operation of the inlets.


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    Titel :

    Factors Controlling Air-Inlet Flow Distortions


    Beteiligte:

    Erscheinungsdatum :

    1956


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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