An engine inlet for efficient operation at both design Mach number and off-design Mach numbers with an inlet having a caret configuration with rotatably extending effective leading edges on the inlet from a retracted position aligned with a nominal Mach number shock wave to an extended position aligned with an off-design Mach number shock wave.


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    Title :

    SUPERSONIC CARET INLET SYSTEM LEADING EDGE SLAT FOR IMPROVED INLET PERFORMANCE AT OFF-DESIGN FLIGHT CONDITIONS


    Additional title:

    ÜBERSCHALL-EINLASSSYSTEMVORDERKANTENKLAPPE FÜR VERBESSERTE EINLASSLEISTUNG BEI OFF-DESIGN FLUGBEDINGUNGEN
    BEC DE BORD D'ATTAQUE DE SYSTÈME D'ENTRÉE DE CARET SUPERSONIQUE POUR UNE MEILLEURE PERFORMANCE D'ENTRÉE DANS DES CONDITIONS DE VOL NON NOMINALES


    Contributors:
    HUYNH THUY (author)

    Publication date :

    2018-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS