Extension of manned, maneuvering flight into Mach 2-3 regime disclosed series inlet/engine compatibility problems not adequately predicted by analysis or laboratory testing; extension of operational flight to Mach 3.5 or 4.5 by future aircraft will amplify compatibility problems; fundamental problems of inlet/ engine system involve airflow matching, pressure distortion, and unsteady flow; in all cases, increasing design Mach number increases severity of these problems and will place greater demands upon all components of propulsion system; some guidelines for compatibility program are outlined showing that five test conditions can give high degree of assurance of relatively trouble-free and successful flight test program.


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    Titel :

    Integration of inlet and engine -- Engine man's point of view


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Cotter, H.N. (Autor:in)

    Kongress:

    SAE Meeting ; 1968 Inlets



    Erscheinungsdatum :

    1968


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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    Randall, L.M. / Hand, W.H. | Engineering Index Backfile | 1968


    Integration of Inlet and Engine — An Airplane Man’s Point of View

    Randall, L. M. / Hand, W. H. | SAE Technical Papers | 1968


    Inlets and Inlet/Engine Integration

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    ENGINE INLET

    LAMB DONALD WILLIAM JR / SIMONETTI JOSEPH LAWRENCE | Europäisches Patentamt | 2019

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