10,000-hp tunnel, inaugurated at Whitley works of W.G. Armstrong Whitworth Aircraft Ltd, Coventry, capable of testing models 16 in. long in Mach number range 0.3 to 3.0; it will be used for investigating rockets, advanced jet engines, guided missiles and future high speed aircraft; Schlieren camera used for photographing air flow patterns. (See also Engineering v 179 n 4665 June 24 1955 p 797-800, v 180 n 4666 July 1 p 25-7)


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    Titel :

    Continuous supersonic wind tunnel


    Weitere Titelangaben:

    Engineer


    Erschienen in:

    Engineer ; 199 , n 5187


    Erscheinungsdatum :

    1955


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    High supersonic wind tunnel

    Engineering Index Backfile | 1961


    High supersonic wind tunnel

    Engineering Index Backfile | 1961


    High supersonic wind tunnel

    Engineering Index Backfile | 1961


    Supersonic wind tunnel optimization

    BUSHNELL, D. / TRIPI, R. | AIAA | 1986


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959