Simplified procedure has been developed to aid in reduction of data obtained by tailpipe or nozzle instrumentation; equations are derived from which working curves may be plotted to show clearly effect of changes in any variable; these curves are especially useful in flight test data reduction.


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    Title :

    Determination of turbojet engine thrust from tailpipe measurements


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Pyle, R.W. (author)

    Published in:

    Publication date :

    1947


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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