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Numerical Investigation of Thrust-Reversing Nozzles
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S.M. Liang,
Published/Copyright:
December 1, 1991
Published Online: 1991-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
- Prediction of Airfoil Separated Flow Unsteady Aerodynamics
- Numerical Investigation of Thrust-Reversing Nozzles
- Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
- System Design Aspects of Propulsion Education in Aerospace Engineering Curricula
Articles in the same Issue
- CONTENTS
- Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
- Prediction of Airfoil Separated Flow Unsteady Aerodynamics
- Numerical Investigation of Thrust-Reversing Nozzles
- Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
- System Design Aspects of Propulsion Education in Aerospace Engineering Curricula
