Influence of Unsteadiness on the Analysis of Pressure Gain Combustion Devices
Author(s) -
Daniel E. Paxson,
Tom Kaemming
Publication year - 2014
Publication title -
journal of propulsion and power
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.913
H-Index - 101
eISSN - 1533-3876
pISSN - 0748-4658
DOI - 10.2514/1.b34913
Subject(s) - ramjet , combustion , thrust , momentum (technical analysis) , energy conservation , thermodynamic cycle , turbofan , turbine , mechanics , aerospace engineering , thermal efficiency , mechanical engineering , engineering , physics , combustor , chemistry , electrical engineering , organic chemistry , finance , economics
Pressure gain combustion has been the subject of scientific study for over a century due to its promise of improved thermodynamic efficiency. In many recent application concepts, pressure gain combustion is used as a component in an otherwise continuous, normally steady flow system, such as a gas turbine or ramjet engine. However, pressure gain combustion is inherently unsteady. Failure to account for the effects of this periodic unsteadiness can lead to misunderstanding and errors in some performance calculations. This paper clarifies the accounting by presenting a consistent method of thermodynamic cycle analysis for a device using pressure gain combustion technology. The incorporation of the unsteady pressure gain combustion process into the conservation equations for a continuous flow device is presented. Most important, the appropriate method for computing the conservation of momentum is presented. It will be shown that proper, consistent analysis of cyclic conservation principles produces more reali...
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