Pressure measurements made on right upper wing extended to include portions affected by slip stream, fuselage, and windshield, left lower wing, and tail surfaces of Boeing PW-9 airplane, simultaneously with accelerometer readings at center of gravity, wing tip and tail in maneuvers; report is for purpose of making this collection of airplane-load data available to those interested in airplane structures.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Pressure distribution over wings and tail surfaces of PW-9 pursuit airplane in flight


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:
    Rhode, R.V. (author)


    Publication date :

    1930


    Size :

    103 pages


    Remarks:

    103 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :