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Impact of a Variable Cycle Engine on Conceptual Aircraft Sizing
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Vivek Sanghi,
Published/Copyright:
March 1, 2003
Published Online: 2003-03
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors
- The Effects of Vibrating Blades on Turbomachinery Rotor-Stator Interaction
- Effects of Shock-Wave on Flow Structure in Tip Region of Transonic Compressor Rotor
- Control of Suddenly Expanded Flows with Micro-Jets
- Impact of a Variable Cycle Engine on Conceptual Aircraft Sizing
Articles in the same Issue
- CONTENTS
- A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors
- The Effects of Vibrating Blades on Turbomachinery Rotor-Stator Interaction
- Effects of Shock-Wave on Flow Structure in Tip Region of Transonic Compressor Rotor
- Control of Suddenly Expanded Flows with Micro-Jets
- Impact of a Variable Cycle Engine on Conceptual Aircraft Sizing
