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; Engineer v 197 n 5133 June 11 1954 p 864-6; Flight v 65 n 2367 June 4 1954 p 734-6)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Transonic and low-speed wind tunnels


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 86 , n 2238


    Publication date :

    1954


    Size :

    4 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


    Transonic Wind Tunnels

    Chanetz, Bruno / Délery, Jean / Gilliéron, Patrick et al. | Springer Verlag | 2020


    Towards New Transonic Wind Tunnels

    J. P. Hartzuiker | NTIS | 1979