Increasing performance requirements have escalated the cost of recent tactical aircraft. Reducing the cost of future aircraft requires accurate evaluation of interactions between performance capability, life cycle cost, and weapon system effectiveness early in the development cycle. This necessitates consideration of a large matrix of candidate systems and, thus, requires a systematic and economical procedure for design selection. An approach for engine selection has been developed which considers these interactions in conjunction with mission and armament requirements and projected threat. This paper discusses the engine selection procedure and presents typical results. Procedures for incorporation of early predictions of engine life and usage impact on total system life cycle cost are also discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Advanced design procedure for aircraft engine selection


    Weitere Titelangaben:

    Fortschrittliche Konstruktionsverfahren fuer Flugzeugtriebwerke


    Beteiligte:
    Eschweiler, J. (Autor:in) / Glaser, F.C. (Autor:in) / Martens, R.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1977


    Format / Umfang :

    9 Seiten, 16 Bilder, 7 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Advanced design procedure for aircraft engine selection

    ESCHWEILER, J. / GLASER, F. / MARTENS, R. | AIAA | 1977


    Aircraft design procedure

    Lickley, R.L. | Engineering Index Backfile | 1948


    Aircraft design procedure

    Lickley, R.L. | Engineering Index Backfile | 1948


    Advanced Stratified Charge Rotary Aircraft Engine Design Study

    P. Badgley / M. Berkowitz / C. Jones et al. | NTIS | 1982


    Advanced stratified charge rotary aircraft engine design study

    Badgley, P. / Berkowitz, M. / Jones, C. et al. | NTRS | 1982