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 - v 179 n 4665 June 24 1955 p 797-800; Engineer v 199 n 5187 June 24 1955 p 871-4)


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    Titel :

    Continuous supersonic wind tunnel


    Weitere Titelangaben:

    Engineering


    Erschienen in:

    Engineering ; 180 , n 4666


    Erscheinungsdatum :

    1955


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Continuous supersonic wind tunnel

    Engineering Index Backfile | 1955


    Supersonic wind tunnel optimization

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


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959