Development of a Multiobjective Optimization Method for Aerospace Turbopump Design

Ernesto Benini,; Marco Cenzon,

doi:10.1515/TJJ.2010.27.3-4.219

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Development of a Multiobjective Optimization Method for Aerospace Turbopump Design

Ernesto Benini, und Marco Cenzon,

Veröffentlicht/Copyright: 1. Dezember 2010

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 27 Heft 3-4

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MLA
APA
Harvard
Chicago
Vancouver

Benini,, Ernesto and Cenzon,, Marco. "Development of a Multiobjective Optimization Method for Aerospace Turbopump Design" International Journal of Turbo and Jet Engines, vol. 27, no. 3-4, pp. 219-250. https://doi.org/10.1515/TJJ.2010.27.3-4.219

Benini,, E. & Cenzon,, M. (). Development of a Multiobjective Optimization Method for Aerospace Turbopump Design. International Journal of Turbo and Jet Engines, 27(3-4), 219-250. https://doi.org/10.1515/TJJ.2010.27.3-4.219

Benini,, E. and Cenzon,, M. () Development of a Multiobjective Optimization Method for Aerospace Turbopump Design. International Journal of Turbo and Jet Engines, Vol. 27 (Issue 3-4), pp. 219-250. https://doi.org/10.1515/TJJ.2010.27.3-4.219

Benini,, Ernesto and Cenzon,, Marco. "Development of a Multiobjective Optimization Method for Aerospace Turbopump Design" International Journal of Turbo and Jet Engines 27, no. 3-4 (): 219-250. https://doi.org/10.1515/TJJ.2010.27.3-4.219

Benini, E, Cenzon, M. Development of a Multiobjective Optimization Method for Aerospace Turbopump Design. International Journal of Turbo and Jet Engines. ;27(3-4): 219-250. https://doi.org/10.1515/TJJ.2010.27.3-4.219

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Published Online: 2010-12

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Artikel in diesem Heft

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

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https://doi.org/10.1515/TJJ.2010.27.3-4.219

Artikel in diesem Heft

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