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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Inlet and Propulsion Integration of Scram Propelled Vehicles


    Contributors:

    Publication date :

    1996-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Inlet and Propulsion Integration of SCRAM Propelled Vehicles

    Povinelli, L. A. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996



    Inlet and Propulsion Integration of RAM Propelled Vehicles

    Bissinger, N. C. / Advisory Group for Aerospace Research and Development; Fluid Dynamics Panel / Von Karman Institute for Fluid Dynamics | British Library Conference Proceedings | 1996


    Inlet and Propulsion Integration of RAM Propelled Vehicles

    Bissinger, N. C. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996


    Configurational Aerothermodynamics of RAM and SCRAM Propelled Vehicles

    Perrier, P. / Courty, J. C. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996