This report presents and discusses the results of an investigation to develop a rationale and technique for the validation of turbine engine steady-state mathematical models for use in predicting flight test performance, stability, and durability parameters. A validation procedure is derived and demonstrated using the YJ101 prototype engine AEDC test results and status deck as an example application of the technique. Typical status deck uncertainties as a function of flight condition, engine power setting, and deck input parameters are given. Status deck flight test input error effects are also given.


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    Title :

    Turbine engine mathematical model validation


    Additional title:

    Bewertung von Turbomotoren aufgrund mathematischer Modelle


    Contributors:

    Published in:

    Publication date :

    1976


    Size :

    43 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English