The material to be presented in these two lectures begins with cycle considerations of the turbojet engine combined with a ramjet engine to provide thrust over the range of Mach 0 to 5. We will then examine in some detail the aerodynamic behavior that occurs in the inlet operating near the peak speed. Following that, we shall view a numerical simulation through a baseline scramjet engine, starting at the entrance to the inlet, proceeding into the combustor and through the nozzle. In the next segment, we examine a combined rocket and ramjet propulsion system. Analysis and test results will be examined with a view toward evaluation of the concept as a practical device. Two other inlets will then be reviewed: a Mach 12 inlet and a Mach 18 configuration. Finally, we close our lectures with a discussion of the Detonation Wave engine, and inspect the physical and chemical behavior obtained from numerical simulation. A few final remarks will be made regarding the application of CFD for hypersonic propulsion components.
Inlet and Propulsion Integration of Scram Propelled Vehicles
01.10.1996
Aufsatz (Konferenz)
Keine Angabe
Englisch
Inlet and Propulsion Integration of SCRAM Propelled Vehicles
British Library Conference Proceedings | 1996
|Inlet and propulsion integration of RAM propelled vehicles
TIBKAT | 1996
|Inlet and Propulsion Integration of RAM Propelled Vehicles
British Library Conference Proceedings | 1996
|Inlet and Propulsion Integration of RAM Propelled Vehicles
British Library Conference Proceedings | 1996
|Configurational Aerothermodynamics of RAM and SCRAM Propelled Vehicles
British Library Conference Proceedings | 1996
|