Considerations involved in optimizing propulsion package, which includes inlet and exhaust nozzle as well as engine; influence of engine airflow scheduling with Mach number as it affects overall performance and weight of propulsion system is shown; nonmixed flow, duct heating turbofan with Mach-3 cruise capability is selected for study and conical centerbody axisymmetric inlet is assumed.
Propulsion systems for supersonic transports
SAE -- Paper
SAE Meeting ; 1962
1962
6 pages
Conference paper
English
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Propulsion Systems for Supersonic Transports
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