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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    Title :

    Transonic and low-speed wind tunnels


    Additional title:

    Flight


    Published in:

    Flight ; 65 , n 2367


    Publication date :

    1954


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Transonic and low-speed wind tunnels

    Engineering Index Backfile | 1954


    Transonic and low-speed wind tunnels

    Engineering Index Backfile | 1954


    Transonic and low-speed wind tunnels

    Engineering Index Backfile | 1954


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