The Thermal Stability of Aviation Fuel

J.S. Mills,; F.R. Edwards,

doi:10.1515/TJJ.1985.2.1.39

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The Thermal Stability of Aviation Fuel

J.S. Mills, and F.R. Edwards,

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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APA
Harvard
Chicago
Vancouver

Mills,, J.S. and Edwards,, F.R.. "The Thermal Stability of Aviation Fuel" International Journal of Turbo and Jet Engines, vol. 2, no. 1, 1985, pp. 39-44. https://doi.org/10.1515/TJJ.1985.2.1.39

Mills,, J. & Edwards,, F. (1985). The Thermal Stability of Aviation Fuel. International Journal of Turbo and Jet Engines, 2(1), 39-44. https://doi.org/10.1515/TJJ.1985.2.1.39

Mills,, J. and Edwards,, F. (1985) The Thermal Stability of Aviation Fuel. International Journal of Turbo and Jet Engines, Vol. 2 (Issue 1), pp. 39-44. https://doi.org/10.1515/TJJ.1985.2.1.39

Mills,, J.S. and Edwards,, F.R.. "The Thermal Stability of Aviation Fuel" International Journal of Turbo and Jet Engines 2, no. 1 (1985): 39-44. https://doi.org/10.1515/TJJ.1985.2.1.39

Mills, J, Edwards, F. The Thermal Stability of Aviation Fuel. International Journal of Turbo and Jet Engines. 1985;2(1): 39-44. https://doi.org/10.1515/TJJ.1985.2.1.39

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Published Online: 1985-03

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Torsional/Lateral Coupling in Geared Rotors
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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.1985.2.1.39

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