Simulated wing effect on pressure drag coefficient of subsonic boattail at angle of attack


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    Title :

    Effect of a simulated wing on the pressure-drag coefficients of various 15 deg boattails at Mach numbers from 0.56 to 1.00


    Contributors:

    Publication date :

    1968-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :