A method of presenting turbojet-engine air-flow requirements and inlet-system air-flow capacities in identical though independent parametric terms is developed. The application of the air-flow representation technique to the analysis of engine-inlet matching conditions is demonstrated. Several examples are presented to illustrate the application of the method to the explicit determination of inlet geometric variations required to improve the power-plant performance of supersonic airplanes.


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    Titel :

    An analysis of turbojet-engine-inlet matching


    Beteiligte:

    Erscheinungsdatum :

    01.09.1953


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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