The obtaining of gas turbine engine mathematical models from experimental data with identification or refinement of their unit characteristics and the use of such models in parametric diagnostics methods is considered. The solution of improperly posed problems, where the number of equations is not equal to the number of unknowns, is proposed to be solved by a mathematical method specially developed using the stability of estimates.


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    Titel :

    Algorithm for Gas Turbine Engine Diagnostics with the Use of Empirical Mathematical Model


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:
    Ahmed, H. S. (Autor:in) / Osipov, B. M. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 64 , 2 ; 297-304


    Erscheinungsdatum :

    01.04.2021


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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