The effect of supersonic nonuniform freestreams, as may occur in aircraft wakes, on the aerodynamic coefficients of sharp and blunt cones, representing aerodynamic decelerating devices and separating stores, were investigated analytically for employing an extension of the two- and three-dimensional methods of characteristics. The study was limited to inviscid aerodynamics. The effect of angle of attack on the aerodynamic coefficients was investigated. (Author)


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    Title :

    Blunt Cones at Angle of Attack in Supersonic Nonuniform Freestreams


    Contributors:
    C. H. Lewis (author) / R. R. Black (author)

    Publication date :

    1972


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English