A record of excellent compatibility with induction systems of all installations has been established by the J79 engine in six air weapons operating at Mach 2 and above. The paper discusses the aspects of steady state matching, dynamic matching, inflow distortion, and compressor design. Studies show that the engine must be evaluated as a component of the propulsion system, and that dynamic matching is at least as important as steady state matching for air breathing engines at Mach 3 and above.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Davies, D. P. (Autor:in) / Alford, J. S. (Autor:in) / Young, L. C. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1962-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Inlet duct -- Engine airflow match and compatibility for supersonic aircraft

    Alford, J.S. / Davies, D.P. / Young, L.C. | Engineering Index Backfile | 1962


    Engine air inlet compatibility for supersonic transport

    Kepler, C.E. / Barry, F.W. | Engineering Index Backfile | 1965


    Engine Air Inlet Compatibility for the Supersonic Transport

    Kepler, C. Edward / Barry, Frank W. | SAE Technical Papers | 1965