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Bifurcation Analysis for Onset and Cessation of Surge in Axial Flow Compressors
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Anurag Agarwal,
Published/Copyright:
September 1, 2000
Published Online: 2000-09
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Effect of Mach Number on Secondary Flow Characteristics
- Axial Spacing Effects in a Transonic Compressor on the Upstream Vane Loading
- Bifurcation Analysis for Onset and Cessation of Surge in Axial Flow Compressors
- Thrust-Vectoring a Single Impinging Jet in a Crossflow
- Numerical Simulation of Supersonic Slot Injection Into A Turbulent Supersonic Stream
Articles in the same Issue
- CONTENTS
- Effect of Mach Number on Secondary Flow Characteristics
- Axial Spacing Effects in a Transonic Compressor on the Upstream Vane Loading
- Bifurcation Analysis for Onset and Cessation of Surge in Axial Flow Compressors
- Thrust-Vectoring a Single Impinging Jet in a Crossflow
- Numerical Simulation of Supersonic Slot Injection Into A Turbulent Supersonic Stream
