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Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft
ISSN: 0148-7191, e-ISSN: 2688-3627
Published January 01, 1962 by SAE International in United States
Annotation ability available
A record of excellent compatibility with induction systems of all installations has been established by the J79 engine in six air weapons operating at Mach 2 and above. The paper discusses the aspects of steady state matching, dynamic matching, inflow distortion, and compressor design. Studies show that the engine must be evaluated as a component of the propulsion system, and that dynamic matching is at least as important as steady state matching for air breathing engines at Mach 3 and above.
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CitationAlford, J., Davies, D., and Young, L., "Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft," SAE Technical Paper 620300, 1962, https://doi.org/10.4271/620300.
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