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Fighter Aircraft Affordability, Survivability, and Effectiveness Through Multi-Function Thrust-Vectoring Nozzles
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Paul W. Herrick,
Published/Copyright:
March 1, 1992
Published Online: 1992-03
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Basic Analysis of Counter-Rotating Turbines
- Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
- Fighter Aircraft Affordability, Survivability, and Effectiveness Through Multi-Function Thrust-Vectoring Nozzles
- Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor
- Influences of Inlet Conditions on Flow Distortion in a Circular-to-Rectangular Transition Duct
Articles in the same Issue
- CONTENTS
- Basic Analysis of Counter-Rotating Turbines
- Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
- Fighter Aircraft Affordability, Survivability, and Effectiveness Through Multi-Function Thrust-Vectoring Nozzles
- Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor
- Influences of Inlet Conditions on Flow Distortion in a Circular-to-Rectangular Transition Duct
