Modeling of Radiation Heat Transfer in Liquid Rocket Engines

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Effects of radiation on the coolantstagnation temperature of the SSMECoolant Stagnation Temperature (R)700600500400300200100-15 -10 -5 0 5 10Axial Position (in)No radiationWith Radiation, HITRANWith Radiation, HITEMP
Effects of radiation on coolantstagnation pressure of SSME70006500Coolant Stagnation Pressure (psi)600055005000With Radiation, HITEMPWith Radiation, HITRANNo Radiation45004000-15 -10 -5 0 5 10Axial Position (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: Effects of radiation on the walltem
Page 19 and 20: Contour of the RP1-LOX engine108Lin
Page 21 and 22: Effects of radiation on the walltem
Page 23 and 24: Effects of radiation on the coolant
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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