Principles of inlet design with emphasis on problems of matching inlets to turbojet engines; wind tunnel performance characteristics; specific design which incorporates both variable throat and capture area, illustrates capabilities of variable geometry design; consideration of closed loop and schedule controls.


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    Titel :

    Performance and control of variable geometry aircraft inlets


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Maravel, J.H. (Autor:in) / Lyttle, J. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1958 Air induction



    Erscheinungsdatum :

    1958


    Format / Umfang :

    20 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    PERFORMANCE AND CONTROL OF VARIABLE GEOMETRY AIRCRAFT INLETS

    MARAVEL, JAMES H. / LYTTLE, JOHN | SAE Technical Papers | 1958


    Variable Geometry for Supersonic Mixed-Compression Inlets

    Norman E.Sorensen / Eldon A.Latham / Donald B. Smeltzer | AIAA | 1976


    Variable geometry for supersonic mixed-compression inlets

    Sorensen, N. E. / Latham, E. A. / Smeltzer, D. B. | NTRS | 1974


    Variable geometry for supersonic mixed-compression inlets

    SORENSEN, N. / LATHAM, E. / SMELTZER, D. | AIAA | 1974


    Performance Analysis of Variable-Geometry Scramjet Inlets Using a Low-Order Model

    Dalle, Derek / Torrez, Sean / Driscoll, James | AIAA | 2011