Three missile body shapes tested at Mach numbers of 1.50, 2.16, and 2.86 with angles of attack up to 30 degrees are described. The flow characteristics for each body shape are examined. The measured aerodynamic forces and moments are presented. The use of flow visualization techniques are described and the results such as vortex effects are discussed.


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    Title :

    Investigation of Flow Characteristics over Missile Bodies at Supersonic Speeds


    Contributors:
    R. L. Barger (author) / W. C. Sawyer (author)

    Publication date :

    1979


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English