Wind tunnel of National Advisory Committee for Aeronautics is of the open-jet type with airstream 20 ft. in diam.; jet of air is drawn through open room; tunnel particularly suitable to testing airscrews; fan belt driven by Diesel engine; test chamber 50 by 60 ft. and 55 ft. high with traveling electric crane; new type of balance developed so that full sized fuselages might be tested. Abstract of N.A.C.A. Report No. 300.


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    Title :

    N.A.C.A. 20 ft. propeller research tunnel


    Additional title:

    Aeroplane


    Contributors:
    Weick, F. (author) / Wood, D. (author)

    Published in:

    Aeroplane ; 36 , n 17


    Publication date :

    1929


    Size :

    4 pages


    Remarks:

    3 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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