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.
Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
1962-01-01
Aufsatz (Konferenz)
Englisch
Inlet duct -- Engine airflow match and compatibility for supersonic aircraft
Engineering Index Backfile | 1962
|Engine air inlet compatibility for supersonic transport
Engineering Index Backfile | 1965
|Engine Air Inlet Compatibility for the Supersonic Transport
SAE Technical Papers | 1965
|