Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft

M. Harefors,; D.G. Bates,

doi:10.1515/TJJ.2003.20.2.95

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Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft

M. Harefors, and D.G. Bates,

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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Harefors,, M. and Bates,, D.G.. "Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft" International Journal of Turbo and Jet Engines, vol. 20, no. 2, pp. 95-114. https://doi.org/10.1515/TJJ.2003.20.2.95

Harefors,, M. & Bates,, D. (). Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft. International Journal of Turbo and Jet Engines, 20(2), 95-114. https://doi.org/10.1515/TJJ.2003.20.2.95

Harefors,, M. and Bates,, D. () Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft. International Journal of Turbo and Jet Engines, Vol. 20 (Issue 2), pp. 95-114. https://doi.org/10.1515/TJJ.2003.20.2.95

Harefors,, M. and Bates,, D.G.. "Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft" International Journal of Turbo and Jet Engines 20, no. 2 (): 95-114. https://doi.org/10.1515/TJJ.2003.20.2.95

Harefors, M, Bates, D. Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft. International Journal of Turbo and Jet Engines. ;20(2): 95-114. https://doi.org/10.1515/TJJ.2003.20.2.95

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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.2003.20.2.95

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®