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 wing upper and lower surface chordwise pressure distributions for the nacelles-off configuration.


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    Title :

    Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 6. Wing Chordwise Pressure Distribution - Nacelles Off


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

    Publication date :

    1972


    Size :

    390 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English