Modeling of Radiation Heat Transfer in Liquid Rocket Engines

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Effects of radiation on the coolanttemperature of the RP1-LOXengine450400Coolant temperature, R350300250No RadiationWith Rdiation HITEMP200150-10 -5 0 5Axial location, in
Effects of radiation on the coolantstagnation pressure of the RP1-LOX3000engine2900Coolant stagnation pressure, psi28002700260025002400No radiationWith radiation2300-10 -5 0 5Axial location, in
Page 1 and 2: Modeling of Radiation HeatTransfer
Page 3 and 4: Previous Works• Hammad, K.J., and
Page 5 and 6: Exchange Factors betweengas and sur
Page 7 and 8: Total Exchange FactorsAccount for w
Page 9 and 10: Plank-Mean Properties for CO 20.40.
Page 11 and 12: Absorption Coefficient of SootWhen
Page 13 and 14: Results for a LH2-LO2 Engine(SSME)T
Page 15 and 16: Effects of radiation on the walltem
Page 17 and 18: Effects of radiation on coolantstag
Page 19 and 20: Contour of the RP1-LOX engine108Lin
Page 21: Effects of radiation on the walltem
Page 25 and 26: Concluding Remarks• The effects o
Page 27 and 28: Concluding Remarks• For the RP1/L

Modeling of Radiation Heat Transfer in Liquid Rocket Engines

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