Cogeneration and Multiple Heat Recovery

J. Davidse,; A. P. van Ooststroom,

doi:10.1515/TJJ.1985.2.1.71

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Cogeneration and Multiple Heat Recovery

J. Davidse, and A. P. van Ooststroom,

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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MLA
APA
Harvard
Chicago
Vancouver

Davidse,, J. and van Ooststroom,, A. P.. "Cogeneration and Multiple Heat Recovery" International Journal of Turbo and Jet Engines, vol. 2, no. 1, 1985, pp. 71-80. https://doi.org/10.1515/TJJ.1985.2.1.71

Davidse,, J. & van Ooststroom,, A. (1985). Cogeneration and Multiple Heat Recovery. International Journal of Turbo and Jet Engines, 2(1), 71-80. https://doi.org/10.1515/TJJ.1985.2.1.71

Davidse,, J. and van Ooststroom,, A. (1985) Cogeneration and Multiple Heat Recovery. International Journal of Turbo and Jet Engines, Vol. 2 (Issue 1), pp. 71-80. https://doi.org/10.1515/TJJ.1985.2.1.71

Davidse,, J. and van Ooststroom,, A. P.. "Cogeneration and Multiple Heat Recovery" International Journal of Turbo and Jet Engines 2, no. 1 (1985): 71-80. https://doi.org/10.1515/TJJ.1985.2.1.71

Davidse, J, van Ooststroom, A. Cogeneration and Multiple Heat Recovery. International Journal of Turbo and Jet Engines. 1985;2(1): 71-80. https://doi.org/10.1515/TJJ.1985.2.1.71

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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.1985.2.1.71

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