Details of two new tunnels operated by English Electric Aviation at Wharton, Great Britain, which comprise 4-ft working-section tunnel for speeds from Mach 0.4 to 4.0, and 18-in. tunnel for speeds from Mach 1.5 to Mach 6, complementary to tunnels in existence; Mach 4 tunnel is intended to test characteristics of supersonic aircraft and will be used for work on Lightning fighter TSR-2 and supersonic airliners; Mach 6 tunnel is intended for testing of missiles; air supply system.


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    Titel :

    Supersonic wind tunnels


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Keil, C.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic Wind Tunnels

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


    Diffusers for supersonic wind tunnels

    Lukasiweicz, J. | Engineering Index Backfile | 1953


    New wind tunnels for supersonic flight

    Engineering Index Backfile | 1960



    Supersonic Flow Development in Slotted Wind Tunnels

    M. A. Ramaswamy / E. S. Cornette | AIAA | 1982