2017
DOI: 10.1016/j.ast.2017.04.026
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Experimental study of pyrolysis–combustion coupling in a regeneratively cooled combustor: System dynamics analysis

Abstract: Scramjets are suitable for hypersonic flight, but their use requires the ability to ensure their thermal protection. In this context, a remotely controlled fuel-cooled combustor, suitable for the experimental analysis of the pyrolysis-combustion coupling characterizing a regeneratively cooled combustion chamber when a hydrocarbon propellant is used, has been designed. Similitude rules were used. Ethylene is used as fuel, air as oxidizer, with an equivalence ratio between 1.0 and 1.5 and a fuel injection pressu… Show more

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Cited by 30 publications
(1 citation statement)
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“…The buoyancy and flow acceleration caused by the change in physical parameters have a massive effect on the heat transfer of the fluid [7][8][9]. Under high temperatures, coking and carbon deposition caused by the pyrolysis of hydrocarbon fuel can also cause the blockage of regenerative cooling channels [10][11][12][13][14][15]. The application of the heat released from combustion and aerodynamic heating to the wall surface with unsteady and uneven thermal loads [16][17][18] results in uneven cooling flow distribution.…”
Section: Introductionmentioning
confidence: 99%
“…The buoyancy and flow acceleration caused by the change in physical parameters have a massive effect on the heat transfer of the fluid [7][8][9]. Under high temperatures, coking and carbon deposition caused by the pyrolysis of hydrocarbon fuel can also cause the blockage of regenerative cooling channels [10][11][12][13][14][15]. The application of the heat released from combustion and aerodynamic heating to the wall surface with unsteady and uneven thermal loads [16][17][18] results in uneven cooling flow distribution.…”
Section: Introductionmentioning
confidence: 99%