Numerical analysis on thermal environment of liquid rocket with afterburning under different altitudes
Applied Thermal Engineering(2020)
Abstract
•Afterburning mainly occurs in mixed layer between exhaust gas and air.•There is a slightly change of temperature distribution in the near-field region between frozen and reaction flow.•The raise of temperature in reacting plume increased with the increase in distance from nozzle exit, whereas decreased with the rise in flight height.
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Key words
Afterburning effect,Thermal environment,Chemical mechanism,LH2/LOX rocket,Numerical simulation
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