F-111A and XB-70A aircraft instrumentation systems used to investigate dynamic response within air breathing propulsion systems of supersonic aircraft


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    Title :

    Preliminary flight investigation of dynamic phenomena within air breathing propulsion systems of supersonic aircraft.


    Contributors:

    Conference:

    PROPULSION JOINT SPECIALIST CONFERENCE ; 1968 ; CLEVELAND, OH


    Publication date :

    1968-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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