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Steady-state Performance Simulation of PT6A-62 Turboprop Engine Using SIMULINK®
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Changduk Kong,
Published/Copyright:
June 1, 2003
Published Online: 2003-06
©2011 by Walter de Gruyter GmbH & Co.
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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®
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®
