高温非平衡化学反应对高超声速再入飞行器绕流流场的气动热特性有较大影响。
High temperature chemical non equilibrium phenomena have a great effect on the flow field around a reentry vehicle.
用非平衡统计的概念和方法建立微观机理与宏观性能相结合的热疲劳理论。
A non equilibrium statistical theory of thermal fatigue which connects microscopic mechanism with macroscopic properties is established.
以上结果表明微细非平衡组织的热稳定性与其热历史密切相关。
These results indicate that the thermo-stability of fine non-equilibrium microstructure is tightly related to their history.
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