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Numerical Simulation of Supersonic Plume in a Cowl-Plug Nozzle Configuration
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Tony W. H. Sheu,
Published/Copyright:
December 1, 1999
Published Online: 1999-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Experimental Investigation of the Stator Wake Propagation Inside the Flow Passages of an Axial Gas Turbine Rotor
- Propulsion / Aircraft Integration of Hypersonic Vehicles with Active Thrust-Vectoring and Real-Time Simulation of Dynamic Engine Behaviour
- Sensitivity of Ingnition Delay Time and Temperature to Changes in Turbulence Expressed by Magnussen Parameters
- Applications of Least-Squares Finite Element Methods to Compressible Internal Flows
- Numerical Simulation of Supersonic Plume in a Cowl-Plug Nozzle Configuration
- Charged Particle Detection in Rocket Plumes for Monitoring Engine Distress
Articles in the same Issue
- CONTENTS
- Experimental Investigation of the Stator Wake Propagation Inside the Flow Passages of an Axial Gas Turbine Rotor
- Propulsion / Aircraft Integration of Hypersonic Vehicles with Active Thrust-Vectoring and Real-Time Simulation of Dynamic Engine Behaviour
- Sensitivity of Ingnition Delay Time and Temperature to Changes in Turbulence Expressed by Magnussen Parameters
- Applications of Least-Squares Finite Element Methods to Compressible Internal Flows
- Numerical Simulation of Supersonic Plume in a Cowl-Plug Nozzle Configuration
- Charged Particle Detection in Rocket Plumes for Monitoring Engine Distress
