Artikel
Lizenziert
Nicht lizenziert
Erfordert eine Authentifizierung
Computational Studies on Flow Through De Laval Nozzle
-
C. Manisankar,
Veröffentlicht/Copyright:
1. Dezember 2006
Published Online: 2006-12
©2011 by Walter de Gruyter GmbH & Co.
Sie haben derzeit keinen Zugang zu diesem Inhalt.
Sie haben derzeit keinen Zugang zu diesem Inhalt.
Artikel in diesem Heft
- 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
Artikel in diesem Heft
- 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
