Work commenced at site near Bedford, on large tunnel capable of testing models at Mach number of up to 1.3, i.e., 1000 mph at sea level; designed by Aircraft Research Assn for development work on new designs; tunnel speed varied by flaps on guide vanes; models pre-erected on support balance. (See also Engineering v 177 n 4593 Feb 5 1954 p 188; Engineer v 197 n 5115 Feb 5 1954 p 205-6)


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    Title :

    Transonic wind tunnel


    Additional title:

    Aircraft Production


    Published in:

    Publication date :

    1954


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Transonic wind tunnel

    Engineering Index Backfile | 1954


    Transonic wind tunnel

    Engineering Index Backfile | 1954


    Optimum transonic wind tunnel

    BARNWELL, R. / EDWARDS, C. / KILGORE, R. et al. | AIAA | 1986


    Transonic wind tunnel testing

    Goethert, Bernhard H. | TIBKAT | 1961


    Transonic wind tunnel testing

    Goethert, Bernhard H. | SLUB | 1961