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, on 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. (Se)


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    Title :

    Regression simulation of turbine engine performance/aircraft regression model


    Additional title:

    Regressions-Simulation des Betriebsverhaltens von Turbinen - Regressionsmodell fuer Flugzeuge


    Contributors:
    Joy, W. (author) / Mehling, D.E. (author)

    Published in:

    Publication date :

    1978


    Size :

    76 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





    Regression techniques applied to parametric turbine engine simulations

    Ruble, J.R. / Sulkoske, R.A. / Clark, R.E. | Tema Archive | 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 | European Patent Office | 2022

    Free access