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Real Gas Effects on the Performance of Hydrocarbon-Fueled Pulse Detonation Engines
Author(s) -
Louis A. Povinelli,
Shaye Yungster
Publication year - 2003
Publication title -
41st aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2003-712
Subject(s) - detonation , hydrocarbon , environmental science , petroleum engineering , pulse (music) , nuclear engineering , automotive engineering , aerospace engineering , materials science , engineering , chemistry , electrical engineering , explosive material , organic chemistry , voltage
This paper presents results for a single-pulse detonation tube wherein the effects of high temperature dissociation and the subsequent recombination influence the sensible heat release available for providing propulsive thrust. The study involved the use of ethylene and air at equivalence ratios of 0.7 and 1.0. The real gas effects on the sensible heat release were found to be significantly large so as to have an impact on the thrust, impulse and fuel consumption of a PDE.

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