Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider
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Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider
Vol. 28, Issue 7, (2013)
作者机构:
国防科学技术大学 航天与材料工程学院,长沙,410073
作者简介:
基金信息:
DOI:
CLC:
Published:2013
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CHENG Xing-hua, YANG Tao, FENG Zhi-wei. Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider[J]. 2013, 28(7).
DOI:
CHENG Xing-hua, YANG Tao, FENG Zhi-wei. Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider[J]. 2013, 28(7).DOI:
Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider
the loose coupling algorithm was applied to drive the iteration of the aeroheating and heat transfer analysis. Then
the coupling characteristics of aeroheating-temperature field were studied. The results show that
before radiative equilibrium
the errors of cold wall and radiative equilibrium aeroheating are +55.1% and -15.4% over actual aeroheating respectively
so coupling analysis for aeroheating-temperature field was required. As the local adiabatic wall temperature is not changed with time
the surface heat-transfer coefficient is a key parameter for coupling effect. Only two aeroheating calculations are needed during calculation of coupling aeroheating-temperature field with average heat convection coefficient
and the error of predicted wall temperature is less than 2.5%
thus highly improving the analysis efficiency of coupled aeroheating-temperature field.
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