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Inverse Generation of Gas Turbine Component Performance Maps From Experimental Test Data
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Changduk Kong,
Published/Copyright:
June 1, 2010
Published Online: 2010-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Effects of Unsteady Downstream Conditions on the Gas Flow through a Sonic Nozzle
- Experimental Research of a Pulse Detonation Rocket System
- Experimental Investigations of a Pulse Detonation Combustor Integrated with a Turbine
- Inverse Generation of Gas Turbine Component Performance Maps From Experimental Test Data
Articles in the same Issue
- CONTENTS
- Effects of Unsteady Downstream Conditions on the Gas Flow through a Sonic Nozzle
- Experimental Research of a Pulse Detonation Rocket System
- Experimental Investigations of a Pulse Detonation Combustor Integrated with a Turbine
- Inverse Generation of Gas Turbine Component Performance Maps From Experimental Test Data
