Wind tunnel tests on conical boattails, nacelles, and rectangular wings


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effect of a rectangular simulated wing on the pressure-drag coefficient of various boat tails at Mach numbers from 0.60 to 1.47


    Contributors:

    Publication date :

    1969-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :