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First published January 1, 2000

Determination of the optimum performance of gas turbines

Abstract

Earlier analytical and graphical treatments of gas turbine performance, assuming the working fluid to be a perfect gas, are developed to allow for ‘non-perfect’ gas effects and pressure losses. The pressure ratios for maximum power and maximum thermal efficiency are determined analytically; the graphical presentations of performance based on the earlier approach are also modified. It is shown that the optimum conditions previously determined from the ‘air standard’ analyses may be changed quite substantially by the inclusion of the ‘real’ effects.

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References

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Published In

Article first published: January 1, 2000
Issue published: January 1, 2000

Key Words

  1. gas turbines
  2. cycles
  3. optimum conditions
  4. efficiency
  5. specific work
  6. real gas effects
  7. pressure losses

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© 2000 Institution of Mechanical Engineers.

Authors

Affiliations

J. H. Horlock
University of Cambridge Whittle Laboratory UK
W. A. Woods
London University Queen Mary and Westfield College UK

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This article was published in Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science.

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