The aerodynamic characteristics for a winged and wingless cruciform missile configuration were examined. The configuration had an ogive-cylinder body with a 3.5 caliber forebody; an overall length-to-diameter ratio of 11.667; and had cruciform tails that were trapezoidal in planform. Tests were made both with and without 72.9 degree cruciform delta wings. The investigation was made for Mach numbers from 1.50 to 4.63, roll attitudes of 0 degrees and 45 degrees, angles of attack from -4 degrees to 22 degrees, and tail control deflections from 10 degrees to -40 degrees.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wings


    Contributors:

    Publication date :

    1983-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :