Drag of closed cockpit and transport type windshields was determined from tests made at speeds corresponding to Mach number range of approximately 0.25 to 0.58 in NACA 8-ft high speed wind tunnel.


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    Title :

    Investigation of drag of windshields in 8-foot high-speed wind tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1942


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :





    Wind tunnel tests of fuselages and windshields

    Warner, Edward P. | SLUB | 1925


    Wind tunnel tests of fuselages and windshields

    Warner, E.P. | Engineering Index Backfile | 1925