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Free-Jet Testing of a Supersonic Engine/Intake Combination
Published online by Cambridge University Press: 04 July 2016
Extract
The design and development of aircraft powerplants for sustained supersonic operation proves to be an exacting task which involves careful balancing of the requirements for high installed performance and system viability. The latter question may be dominated by the need to ensure flow compatibility at the intake/engine interface.
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- Symposium on Altitude Testing
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- Copyright © Royal Aeronautical Society 1970
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