This report presents the results of wind tunnel pressure distribution measurements made on a model of the Boeing supersonic transport configuration during design of the prototype airplanes. This volume contains vertical tail net chordwise pressure distributions and isobars showing the effect of sideslip and rudder deflections.


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    Title :

    Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. volume 12. Vertical Tail Net Chordwise Pressure Distributions and Isobars


    Contributors:
    M. E. Manro (author) / J. P. Moulijn (author) / J. D. Knittel (author)

    Publication date :

    1972


    Size :

    488 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English