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Development of a Multiobjective Optimization Method for Aerospace Turbopump Design
-
Ernesto Benini,
Published/Copyright:
December 1, 2010
Published Online: 2010-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Computer Simulation of Performance and Economic Assessment of a Single Shaft Gas Turbine Combined Heat Cooling and Power Plant
- Performance Assessment of Single and Two Shaft Gas Industrial Turbines Using Fuels of Different Calorific Values
- Power Conversion System Considerations for an Advanced Nuclear Gas Turbine (GT-VHTR) CHHP Demonstration Plant Concept
- Development of a Multiobjective Optimization Method for Aerospace Turbopump Design
- A Mixed Data-Driven and Model Based Fault Classification for Gas Turbine Diagnosis
- Startup Simulation of Twin Spool Turbofan Engine
- A Computational Investigation of Icing Effects on an S-Duct Inlet
Articles in the same Issue
- CONTENTS
- Computer Simulation of Performance and Economic Assessment of a Single Shaft Gas Turbine Combined Heat Cooling and Power Plant
- Performance Assessment of Single and Two Shaft Gas Industrial Turbines Using Fuels of Different Calorific Values
- Power Conversion System Considerations for an Advanced Nuclear Gas Turbine (GT-VHTR) CHHP Demonstration Plant Concept
- Development of a Multiobjective Optimization Method for Aerospace Turbopump Design
- A Mixed Data-Driven and Model Based Fault Classification for Gas Turbine Diagnosis
- Startup Simulation of Twin Spool Turbofan Engine
- A Computational Investigation of Icing Effects on an S-Duct Inlet
