Data presented through Mach number range from 0.60 to 1.18 and Reynolds number from 2.3 to 5.5 million; results obtained by forced oscillation technique in which electrohydraulic servo valve was used to power drive system.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental wind-tunnel investigation of transonic damping-in-pitch characteristics of two wing-body combinations


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1958


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :