Review of some of design parameters that were considered in integration of induction system, secondary air system, jet nozzle and basic turbojet gas generator for SST by General Electric Co; most important gains in propulsion efficiency have resulted from development of inlets, engines and exhaust nozzles which are matched over broad range of operating conditions; only steady-state matching of inlets, engines and exhaust nozzles is reviewed; significant step in providing high performance as well as high reliability and minimum complexity is use of secondary air pressure to control exit area of nozzle; combined analytical and experimental program demonstrated feasibility of this design feature.
Inlet duct-engine exhaust nozzle airflow matching for supersonic transport
Aeronautical J
Aeronautical Journal ; 72 , n 690
1968
8 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Inlet duct -- Engine airflow match and compatibility for supersonic aircraft
Engineering Index Backfile | 1962
|Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft
SAE Technical Papers | 1962
|Engine/Inlet Matching for Supersonic Aircraft Design
AIAA | 2016
|