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Theoretical Calculation of Stability for NASA Stage 57 Rotor
-
Efrén M. Benavides,
Published/Copyright:
June 1, 2009
Published Online: 2009-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Experimental Study on a Two-phase Pulse Detonation Rocket Engine at the Frequency of 35Hz
- Theoretical Calculation of Stability for NASA Stage 57 Rotor
- Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine
- An Integrated Approach to Gas Turbine Monitoring and Diagnostics
- Microturbine Performance Testing using Biodiesel
- Relationship between Shock-cell Length and Noise of Jets from Rectangular and Elliptic Disk Nozzles
Articles in the same Issue
- CONTENTS
- Experimental Study on a Two-phase Pulse Detonation Rocket Engine at the Frequency of 35Hz
- Theoretical Calculation of Stability for NASA Stage 57 Rotor
- Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine
- An Integrated Approach to Gas Turbine Monitoring and Diagnostics
- Microturbine Performance Testing using Biodiesel
- Relationship between Shock-cell Length and Noise of Jets from Rectangular and Elliptic Disk Nozzles
