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RESEARCH PAPERS: Advanced Energy Systems

Pressure-Gain Combustion: Part II—Experimental and Model Results

[+] Author and Article Information
G. A. Richards, R. S. Gemmen

U.S. Department of Energy, Morgantown Energy Technology Center, Morgantown, WV 26507-0880

J. Eng. Gas Turbines Power 118(3), 469-473 (Jul 01, 1996) (5 pages) doi:10.1115/1.2816669 History: Received October 27, 1994; Revised October 10, 1995; Online November 19, 2007

Abstract

An experimental investigation of aerovalve pulse combustion is presented. The experimental measurements compare favorably with model predictions from a control volume analysis of the pulse combustor. Particular emphasis is placed on the mean pressure differences through the combustor as an indicator of the so-called pressure gain performance. Both the operating conditions and combustor geometry are investigated. It is shown that complex fluid/combustion interactions within the combustor make it difficult to isolate the effect of geometric changes. A scaling rule developed from the control-volume analysis is used to produce a combustor geometry capable of producing pressure gain.

Copyright © 1996 by The American Society of Mechanical Engineers
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