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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    Titel :

    Investigation of pressure-loss characteristics of turbojet inlet screen


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Lankford, J.L. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    7 pages


    Anmerkungen:

    19 Supp sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    Analysis of turbojet-engine-inlet matching

    Wyatt, D.D. | Engineering Index Backfile | 1953