The split-skirt is a variable drag bomb stabilizer which is being studied by the U. S. Naval Ordnance Laboratory. This report gives the results of static and dynamic wind-tunnel tests of several configurations formed from various combinations of three noses and four skirts. (Author)


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    Title :

    The Aerodynamic Characteristics of an Ogive Cylinder with Split-Skirt Stabilizer at Subsonic, Transonic and Supersonic Speeds


    Contributors:
    F. J. Regan (author)

    Publication date :

    1965


    Size :

    79 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English