Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft

620300

01/01/1962

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
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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DOI
https://doi.org/10.4271/620300
Pages
11
Citation
Alford, 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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Publisher
Published
Jan 1, 1962
Product Code
620300
Content Type
Technical Paper
Language
English