Investigation indicates that, except at very low flow rates, static pressure losses increase and total pressure variations become more pronounced with increasing weight flow; smoothing and rounding leading edges of screen vanes caused marked decreases in static pressure loss coefficients and slightly improved total pressure patterns.


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    Title :

    Investigation of pressure-loss characteristics of turbojet inlet screen


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    7 pages


    Remarks:

    19 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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