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Integration of the Brayton and Rankine Cycle to Maximize Gas Turbine Performance — A Cogeneration Option
-
R.L. Messerlie,
and J.R. Strother,
Published/Copyright:
June 1, 1985
Published Online: 1985-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- An Experimental Study of Local and Mean Heat Transfer in a Triangular-Sectioned Duct Rotating in the Orthogonal-Mode
- The Effects of Freestream Turbulence on the Profile Boundary Layer and Losses in a Compressor Cascade
- Integration of the Brayton and Rankine Cycle to Maximize Gas Turbine Performance — A Cogeneration Option
- Dynamic Behavior of Turbulent Flow in a Widely-Spaced Co-Axial Jet Diffusion Flame Combustor
- The Britalus Brayton Cycle Engine
- Power Scaling Characteristics of a Displacement Brayton Cycle Engine
- Port Passage Losses in Britalus Compressors and Expanders
- Fuel Performance Evaluation for the Solid-Fueled Ramjet
- Computer Calculation of Fan Erosion in Coal-Fired Power Plants. Part 1: Centrifugal Fans
Articles in the same Issue
- CONTENTS
- An Experimental Study of Local and Mean Heat Transfer in a Triangular-Sectioned Duct Rotating in the Orthogonal-Mode
- The Effects of Freestream Turbulence on the Profile Boundary Layer and Losses in a Compressor Cascade
- Integration of the Brayton and Rankine Cycle to Maximize Gas Turbine Performance — A Cogeneration Option
- Dynamic Behavior of Turbulent Flow in a Widely-Spaced Co-Axial Jet Diffusion Flame Combustor
- The Britalus Brayton Cycle Engine
- Power Scaling Characteristics of a Displacement Brayton Cycle Engine
- Port Passage Losses in Britalus Compressors and Expanders
- Fuel Performance Evaluation for the Solid-Fueled Ramjet
- Computer Calculation of Fan Erosion in Coal-Fired Power Plants. Part 1: Centrifugal Fans