Advantages and disadvantages of some systems pointed out; test stand described with cold wind tunnel cooling is compared with installation with cooling of combustion air only and suction of exhaust gas; Fiat and DVL test stands described.


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    Title :

    Test stands for altitude study of airplane engines


    Additional title:

    Pruefstaende fuer Hoehenuntersuchungen


    Contributors:


    Publication date :

    1938


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German




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