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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    Title :

    Factors Controlling Air-Inlet Flow Distortions


    Contributors:

    Publication date :

    1956


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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