Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach

Changduk Kong,; Jayoung Ki,; Taekhyeon Kim,

doi:10.1515/TJJ.2003.20.2.171

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Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach

Changduk Kong, , Jayoung Ki, and Taekhyeon Kim,

Published/Copyright: June 1, 2003

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From the journal International Journal of Turbo and Jet Engines Volume 20 Issue 2

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APA
Harvard
Chicago
Vancouver

Kong,, Changduk, Ki,, Jayoung and Kim,, Taekhyeon. "Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach" International Journal of Turbo and Jet Engines, vol. 20, no. 2, pp. 171-182. https://doi.org/10.1515/TJJ.2003.20.2.171

Kong,, C., Ki,, J. & Kim,, T. (). Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach. International Journal of Turbo and Jet Engines, 20(2), 171-182. https://doi.org/10.1515/TJJ.2003.20.2.171

Kong,, C., Ki,, J. and Kim,, T. () Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach. International Journal of Turbo and Jet Engines, Vol. 20 (Issue 2), pp. 171-182. https://doi.org/10.1515/TJJ.2003.20.2.171

Kong,, Changduk, Ki,, Jayoung and Kim,, Taekhyeon. "Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach" International Journal of Turbo and Jet Engines 20, no. 2 (): 171-182. https://doi.org/10.1515/TJJ.2003.20.2.171

Kong, C, Ki, J, Kim, T. Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach. International Journal of Turbo and Jet Engines. ;20(2): 171-182. https://doi.org/10.1515/TJJ.2003.20.2.171

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Articles in the same Issue

CONTENTS
Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft
Gust Response Analysis of a Turbine Cascade
Three Dimensional Navier-Stokes Analysis of a Rigid Wing Configuration
Probabilistic Analysis of Gas Turbine Field Performance
Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section
Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor
Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach
Steady-state Performance Simulation of PT6A-62 Turboprop Engine Using SIMULINK®

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https://doi.org/10.1515/TJJ.2003.20.2.171

Articles in the same Issue

CONTENTS
Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft
Gust Response Analysis of a Turbine Cascade
Three Dimensional Navier-Stokes Analysis of a Rigid Wing Configuration
Probabilistic Analysis of Gas Turbine Field Performance
Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section
Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor
Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach
Steady-state Performance Simulation of PT6A-62 Turboprop Engine Using SIMULINK®