The Aircraft Regression Model (ARM) Task has explored modification of the Boeing Turbine Engine Variable Cycle Selection /Airplane Response Engine Selection(TEVCS/ARES) procedures by decoupling the representation of specific propulsion systems and the detailed mission definitions from the overall surface fit representations of the aircraft. Detailed comparisons between the RSTEP/ARM techniques developed herein and another available technique for aircraft/engine design refinement are provided as the principal result of this program. All objectives of the RSTEP/ARM effort were attained. A simplified mission performance computer program was developed and tested in the evaluation of two engine cycle concepts, one a turbojet and one a turbofan. The program was simplified by using regression models for airframe geometry, weights, and drags. The program is currently operational in both the Air Force and at two industry sites.


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    Titel :

    Regression Simulation of Turbine Engine Performance/Aircraft Regression Model


    Beteiligte:
    W. Joy (Autor:in) / D. E. Uehling (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    76 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Regression techniques applied to parametric turbine engine simulations

    Ruble, J.R. / Sulkoske, R.A. / Clark, R.E. | Tema Archiv | 1980


    Regression techniques applied to parametric turbine engine simulations

    RUBLE, J. / SULKOSKE, R. / CLARK, R. | AIAA | 1980


    AIRCRAFT TURBINE ENGINE

    SERVANT REGIS EUGENE HENRI / DESOMBRE DIDIER GABRIEL BERTRAND / JACQUEMARD CHRISTOPHE PAUL | Europäisches Patentamt | 2022

    Freier Zugriff