This paper presents the results of a fundamental, comprehensive, and rigorous analytical and computational examination of the performance of the Brayton propulsion and power cycle employing real air as the working fluid. This approach capitalizes on the benefits inherent in closed cycle thermodynamic reasoning and the behavior of the thermally perfect gas to facilitate analysis. The analysis uses a high fidelity correlation to represent the specific heat at constant pressure of air as a function of temperature and the polytropic efficiency to evaluate the overall efficiency of the adiabatic compression and expansion processes. The analytical results are algebraic, transparent, and easily manipulated, and the computational results present a useful guidance for designers and users. The operating range of design parameters considered covers any current and foreseeable application. The results include some important comparisons with more simplified conventional analyses.
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November 2011
Research Papers
The Brayton Cycle Using Real Air and Polytropic Component Efficiencies
W. H. Heiser,
W. H. Heiser
Professor of Aeronautics, Emeritus
Life Fellow ASME Honorary Fellow AIAA
U.S. Air Force Academy
, CO 80840
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J. W. Bucey
J. W. Bucey
U.S. Air Force Academy
, CO 80840
Search for other works by this author on:
W. H. Heiser
Professor of Aeronautics, Emeritus
Life Fellow ASME Honorary Fellow AIAA
U.S. Air Force Academy
, CO 80840
T. Huxley
U.S. Air Force Academy
, CO 80840
J. W. Bucey
U.S. Air Force Academy
, CO 80840J. Eng. Gas Turbines Power. Nov 2011, 133(11): 111702 (9 pages)
Published Online: May 17, 2011
Article history
Received:
December 3, 2010
Revised:
February 7, 2011
Online:
May 17, 2011
Published:
May 17, 2011
Citation
Heiser, W. H., Huxley, T., and Bucey, J. W. (May 17, 2011). "The Brayton Cycle Using Real Air and Polytropic Component Efficiencies." ASME. J. Eng. Gas Turbines Power. November 2011; 133(11): 111702. https://doi.org/10.1115/1.4003671
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