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Experimental Investigations on Detonability Limits of Pulse Detonation Rocket Engine
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W. Fan,
Published/Copyright:
December 1, 2006
Published Online: 2006-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Performance Characteristics of a Small-Scale Axial-Type Turbine Operated in a Low Partial Admission Rate
- Computational Studies on Flow Through De Laval Nozzle
- Nozzle Expansion Level Effect on Suddenly Expanded Flow
- Gas Turbine Power Augmentation by Inlet Fogging
- Experimental Investigations on Detonability Limits of Pulse Detonation Rocket Engine
Articles in the same Issue
- CONTENTS
- Performance Characteristics of a Small-Scale Axial-Type Turbine Operated in a Low Partial Admission Rate
- Computational Studies on Flow Through De Laval Nozzle
- Nozzle Expansion Level Effect on Suddenly Expanded Flow
- Gas Turbine Power Augmentation by Inlet Fogging
- Experimental Investigations on Detonability Limits of Pulse Detonation Rocket Engine
