Two tunnels at Warton Aerodrome of British Aircraft Corp are designed to give more accurate information about flying characteristics of future aircraft (such as TSR-2) and missiles (such as Blue Water) than is possible with existing facilities; Mach 0.4 to 4.0 unit has system for simultaneous viewing and photographic recording, working section of 4 ft sq, and can operate at air speeds from 200 to about 3000 mph; Mach 1.5 to 6.0 tunnel has working section of 18 in. sq with speed range of 1150 to 4500 mph.


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    Titel :

    New wind tunnels for supersonic flight


    Weitere Titelangaben:

    Engineering


    Erschienen in:

    Engineering ; 190 , n 4932


    Erscheinungsdatum :

    1960


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic Wind Tunnels

    Keil, C.G. | Emerald Group Publishing | 1960


    Supersonic wind tunnels

    Keil, C.G. | Engineering Index Backfile | 1960


    Diffusers for supersonic wind tunnels

    Lukasiweicz, J. | Engineering Index Backfile | 1953



    Flow direction measurements in supersonic wind tunnels

    Raney, D. J. / Aeronautical Research Council | TIBKAT | 1956