Design of small tunnel test section (4×10-in.) incorporating flexible nozzle; consisting of high strength stepped steel plate; two screw jacks provide easy means of continuously changing nozzle's shape according to aerodynamic requirements; boundary layer compensation can also be varied during operation.


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    Title :

    Flexible nozzle for small supersonic wind tunnel


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Dhawan, S. (author) / Roshko, A. (author)


    Publication date :

    1951


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :