Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity
Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity
复制标题
前向腔钝头体热防护机理的数值研究
DOI:
10.1007/s11431-016-6015-4
复制
发表时间:
2016-01
期刊:
影响因子:
--
通讯作者:
Jiang ZongLin
中科院分区:
文献类型:
--
作者:
Li XinDong;Hu ZongMin;Jiang ZongLin
Numerical experiments are carried out using the standard hypersonic ballistic-type model (HB-2) to investigate the effect of forward-facing cavity on the aerodynamic heating. A general concept is proposed which utilizes the flow disturbances generated passively in the nosed subsonic region to weaken the detached shock wave. Several aspects are mainly studied, including shock shape and standoff distance, surface heat flux and pressure, flowfield feature and cooling mechanism. The numerical results indicate that shock strength and standoff distance increase with an increase in theL/Dratio of the cavity. Interestingly, a bulge structure of the detached shock associated with a deep cavity is observed for the first time. Local surface heat flux and pressure around the concave nose are much lower respectively than those at the stagnation point of the baseline model. In addition, both surface heat and pressure reductions are proportional to theL/Dratio. A negative heating phenomenon may occur in the vicinity of a sharp lip or on the base wall of a deep cavity. If theL/Dratio exceeds 0.7, the detached shock appears as a self-sustained oscillation which can be referred to as the cooling mechanism.
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影响因子:
1.6
作者:
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通讯作者:
L. Huebner;L. Utreja
影响因子:
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作者:
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DOI:
10.2514/6.1994-2050
发表时间:
1994-06
期刊:
--
影响因子:
--
作者:
B. Yuceil;D. Dolling
通讯作者:
B. Yuceil;D. Dolling
DOI:
10.2514/6.1993-2742
发表时间:
1993-07
期刊:
--
影响因子:
--
作者:
B. Yuceil;D. Dolling;D. Wilson
通讯作者:
B. Yuceil;D. Dolling;D. Wilson