Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing engine nacelles at Mach 0.56 to 1.46


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    Title :

    Wind tunnel investigation of airframe installation effects on underwing engine nacelles at Mach numbers from 0.56 to 1.46


    Contributors:

    Publication date :

    1968-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :