Tunnel is of variable density type, designed for pressures from 1/3 to 3 atmospheres at Mach numbers from M-0.3 to M-3.0 on 16-in. long model; reasons behind choice of tunnel. (See also Aeroplane v 88 n 2291 June 17 1955 p 821-5)


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    Title :

    Armstrong Whitworth's new supersonic wind-tunnel


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 67 , n 2421


    Publication date :

    1955


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Armstrong Whitworth's new supersonic wind-tunnel

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