Absorptive, nonreflecting barrier mounted between closely spaced jet engines on supersonic aircraft, for preventing shock wave interference


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    Title :

    Absorptive splitter for closely spaced supersonic engine air inlets Patent


    Contributors:
    Kastan, H. (author)

    Publication date :

    1966-09-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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