Gas Turbine for Pressurising a Fluidised Bed Combustion System

G.H. Dibelius,; R. Croonenbrock,; R.U. Pitt,

doi:10.1515/TJJ.1985.2.1.57

Home Technology Gas Turbine for Pressurising a Fluidised Bed Combustion System

Article

Licensed

Unlicensed Requires Authentication

Gas Turbine for Pressurising a Fluidised Bed Combustion System

G.H. Dibelius, , R. Croonenbrock, and R.U. Pitt,

Published/Copyright: March 1, 1985

Published by

Become an author with De Gruyter Brill

Author Information

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

MLA
APA
Harvard
Chicago
Vancouver

MLA
APA
Harvard
Chicago
Vancouver

Dibelius,, G.H., Croonenbrock,, R. and Pitt,, R.U.. "Gas Turbine for Pressurising a Fluidised Bed Combustion System" International Journal of Turbo and Jet Engines, vol. 2, no. 1, pp. 57-62. https://doi.org/10.1515/TJJ.1985.2.1.57

Dibelius,, G., Croonenbrock,, R. & Pitt,, R. (). Gas Turbine for Pressurising a Fluidised Bed Combustion System. International Journal of Turbo and Jet Engines, 2(1), 57-62. https://doi.org/10.1515/TJJ.1985.2.1.57

Dibelius,, G., Croonenbrock,, R. and Pitt,, R. () Gas Turbine for Pressurising a Fluidised Bed Combustion System. International Journal of Turbo and Jet Engines, Vol. 2 (Issue 1), pp. 57-62. https://doi.org/10.1515/TJJ.1985.2.1.57

Dibelius,, G.H., Croonenbrock,, R. and Pitt,, R.U.. "Gas Turbine for Pressurising a Fluidised Bed Combustion System" International Journal of Turbo and Jet Engines 2, no. 1 (): 57-62. https://doi.org/10.1515/TJJ.1985.2.1.57

Dibelius, G, Croonenbrock, R, Pitt, R. Gas Turbine for Pressurising a Fluidised Bed Combustion System. International Journal of Turbo and Jet Engines. ;2(1): 57-62. https://doi.org/10.1515/TJJ.1985.2.1.57

Copy

Copied to clipboard

BibTeX EndNote RIS

Published Online: 1985-03

You are currently not able to access this content.

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

Search journal Search the content of this journal

https://doi.org/10.1515/TJJ.1985.2.1.57

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