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Change of Surge Margin of a Turboshaft Engine Compressor in Manufacturing Conditions
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Stanislaw Antas,
Veröffentlicht/Copyright:
1. Juni 2001
Published Online: 2001-06
©2011 by Walter de Gruyter GmbH & Co.
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Artikel in diesem Heft
- CONTENTS
- Investigation and Modeling of Mechanical Properties for Thermal Barrier Coatings Under Bending
- Change of Surge Margin of a Turboshaft Engine Compressor in Manufacturing Conditions
- A Parallel Algorithm for Simulation of Unsteady Flows in Multistage Turbomachinery
- Overall Performance Measurements of Annular Combustors Used in P-60 Miniature Turbojet Engine
Artikel in diesem Heft
- CONTENTS
- Investigation and Modeling of Mechanical Properties for Thermal Barrier Coatings Under Bending
- Change of Surge Margin of a Turboshaft Engine Compressor in Manufacturing Conditions
- A Parallel Algorithm for Simulation of Unsteady Flows in Multistage Turbomachinery
- Overall Performance Measurements of Annular Combustors Used in P-60 Miniature Turbojet Engine
