Method of estimating output in flight by means of calibrations based on density of fuel-air mixture in intake pipe is described.


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    Title :

    Aircraft engine power estimation from intake manifold density


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1939


    Size :

    8 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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