Record of excellent compatibility with induction systems of all installations was established by Gen Elec J79 engine in 6 air weapons operating at Mach 2 and above; aspects of steady-state matching, dynamic matching, inflow distortion, and compressor design; studies show that engine must be evaluated as component of propulsion system, and that dynamic matching is as important as steady-state matching for air breathing engines at Mach 3 and above.
Inlet duct -- Engine airflow match and compatibility for supersonic aircraft
SAE -- Paper
SAE Meeting ; 1962 Inlets
1962
10 pages
Conference paper
English
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Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft
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