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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    Title :

    An analysis of turbojet-engine-inlet matching


    Contributors:

    Publication date :

    1953-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English