Record of excellent compatibility with induction systems of all installations was established by Gen Elec J79 engine in 6 air weapons operating at Mach 2 and above; aspects of steady-state matching, dynamic matching, inflow distortion, and compressor design; studies show that engine must be evaluated as component of propulsion system, and that dynamic matching is as important as steady-state matching for air breathing engines at Mach 3 and above.


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    Title :

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


    Additional title:

    SAE -- Paper


    Contributors:
    Alford, J.S. (author) / Davies, D.P. (author) / Young, L.C. (author)

    Conference:

    SAE Meeting ; 1962 Inlets



    Publication date :

    1962


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft

    Davies, D. P. / Alford, J. S. / Young, L. C. | SAE Technical Papers | 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