Inlet-engine compatibility is a recognized major concern in essentially every aircraft development effort. Testing of many configurations throughout the development cycle of a propulsion system is generally required to establish the performance and operational suitability characteristics of a production configuration. A disciplined test methodology based on the use of standardized test techniques is necessary to generate the technical data base required for effective program management decisions. Established test techniques have been developed at the Arnold Engineering Development Center for the systematic and quantitative assessment of turbine engine performance and suitability. A review of the currently available techniques for the evaluation of turbine engine stability is presented. Recommended test matrix selction criteria, instrumentation and test equipment requirements, test procedures, and analysis techniques are discussed with respect to turbine engine testing with three basic engine inlet environmental conditions: uniform, steady flow; steady-state distorted flow; and time-variant distorted flow. (Wassmann)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Inlet-engine compatibility testing techniques in ground test facilities


    Weitere Titelangaben:

    Pruefverfahren fuer die Kompatibilitaet von Einlauf und Triebwerk auf Bodenpruefstaenden


    Beteiligte:
    Tate, J.T. (Autor:in)


    Erscheinungsdatum :

    1981


    Format / Umfang :

    17 Seiten, 19 Bilder, 24 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Inlet-engine compatibility analysis

    CAMPBELL, J. / ELLIS, S. | AIAA | 1970



    F/A-18A inlet/engine compatibility flight test results

    AMIN, N. / HOLLWEGER, D. | AIAA | 1981


    F/A-18 inlet/engine compatibility flight test results

    AMIN, N. F. / HOLLWEGER, D. J. | AIAA | 1983


    Engine/Inlet Compatibility Analysis Procedure

    J. L. CAMPBELL AND S. H. ELLIS | AIAA | 1971