An engine inlet 10 for efficient operation at both design Mach number and off-design Mach numbers has a fixed compression surface 16 and a leading edge 24 that is variably extendible over the fixed compression surface to simultaneously vary capture area, compression and shock wave position.


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    Title :

    VARIABLE-CAPTURE SUPERSONIC INLET


    Additional title:

    ÜBERSCHALLEINLASS MIT VARIABLER ABSAUGUNG
    ENTRÉE SUPERSONIQUE À CAPTURE VARIABLE


    Contributors:
    HUYNH THUY (author) / WILSON DAVID J (author)

    Publication date :

    2021-03-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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