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.
An analysis of turbojet-engine-inlet matching
1953-09-01
Miscellaneous
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English
Analysis of turbojet-engine-inlet matching
Engineering Index Backfile | 1953
|An analysis of turbojet-engine-inlet matching
TIBKAT | 1953
|