Two tunnels completed for de Havilland Aircraft Co at Hatfield; high speed tunnel capable of operation at Mach numbers ranging from 0.8 to 1.6, with working section 2 ft sq, and low speed tunnel for speeds up to 250 ft per sec, capable of accommodating models of 6-ft wing span. (See also Engineering v 177 n 4612 June 18 1954 p 788-91; Aeroplane v 86 n 2238 June 11 1954 p 71-4; Engineer v 197 n 5133 June 11 1954 p 864-6)


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    Titel :

    Transonic and low-speed wind tunnels


    Weitere Titelangaben:

    Flight


    Erschienen in:

    Flight ; 65 , n 2367


    Erscheinungsdatum :

    1954


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Calibration of transonic and supersonic wind tunnels

    Reed, T. D. / Pope, T. C. / Cooksey, J. M. | TIBKAT | 1977



    Generation of Flow Disturbances in Transonic Wind Tunnels

    Medved, B. L. / Vitic, A. | British Library Online Contents | 1992