Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems

J.R. Palmer,; Yah Cheng-Zhong,

doi:10.1515/TJJ.1985.2.1.19

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Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems

J.R. Palmer, and Yah Cheng-Zhong,

Published/Copyright: March 1, 1985

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From the journal International Journal of Turbo and Jet Engines Volume 2 Issue 1

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Palmer,, J.R. and Cheng-Zhong,, Yah. "Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems" International Journal of Turbo and Jet Engines, vol. 2, no. 1, pp. 19-28. https://doi.org/10.1515/TJJ.1985.2.1.19

Palmer,, J. & Cheng-Zhong,, Y. (). Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems. International Journal of Turbo and Jet Engines, 2(1), 19-28. https://doi.org/10.1515/TJJ.1985.2.1.19

Palmer,, J. and Cheng-Zhong,, Y. () Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems. International Journal of Turbo and Jet Engines, Vol. 2 (Issue 1), pp. 19-28. https://doi.org/10.1515/TJJ.1985.2.1.19

Palmer,, J.R. and Cheng-Zhong,, Yah. "Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems" International Journal of Turbo and Jet Engines 2, no. 1 (): 19-28. https://doi.org/10.1515/TJJ.1985.2.1.19

Palmer, J, Cheng-Zhong, Y. Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems. International Journal of Turbo and Jet Engines. ;2(1): 19-28. https://doi.org/10.1515/TJJ.1985.2.1.19

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Published Online: 1985-03

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Articles in the same Issue

CONTENTS
Performance Comparison Between Transpiration Air Cooled Turbine 3000°F (1649°C) Stator Vanes and Solid Uncooled Vanes
Torsional/Lateral Coupling in Geared Rotors
Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems
Turbotest - A Computer Program for Rig Test Analysis of Arbitrary Gas Turbine Engines
The Thermal Stability of Aviation Fuel
Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades
Gas Turbine for Pressurising a Fluidised Bed Combustion System
Double-Decked Gas Turbine with Compact Heat Eschanger
Cogeneration and Multiple Heat Recovery
Simulation of Surge Margin Changes Due to Heat Transfer Effects in Gas Turbine Transients

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https://doi.org/10.1515/TJJ.1985.2.1.19

Articles in the same Issue

CONTENTS
Performance Comparison Between Transpiration Air Cooled Turbine 3000°F (1649°C) Stator Vanes and Solid Uncooled Vanes
Torsional/Lateral Coupling in Geared Rotors
Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems
Turbotest - A Computer Program for Rig Test Analysis of Arbitrary Gas Turbine Engines
The Thermal Stability of Aviation Fuel
Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades
Gas Turbine for Pressurising a Fluidised Bed Combustion System
Double-Decked Gas Turbine with Compact Heat Eschanger
Cogeneration and Multiple Heat Recovery
Simulation of Surge Margin Changes Due to Heat Transfer Effects in Gas Turbine Transients