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Active Control of Surge in Multi-Stage Axial-Flow Compressors
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J.F. Escuret,
Veröffentlicht/Copyright:
1. März 1996
Published Online: 1996-03
©2011 by Walter de Gruyter GmbH & Co.
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Artikel in diesem Heft
- CONTENTS
- Generalized Euler's Turbomachine Equation and Free Vortex Sheet Conditions in Separated/Cavitated Turbo-Flows
- Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow
- Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor
- Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method
- Active Control of Surge in Multi-Stage Axial-Flow Compressors
- Technical Note: Performance of a Miniature Gas Turbine Engine
Artikel in diesem Heft
- CONTENTS
- Generalized Euler's Turbomachine Equation and Free Vortex Sheet Conditions in Separated/Cavitated Turbo-Flows
- Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow
- Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor
- Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method
- Active Control of Surge in Multi-Stage Axial-Flow Compressors
- Technical Note: Performance of a Miniature Gas Turbine Engine
