adj.空气热力学的
The comparison between the gas models appeared great difference for both aerodynamic and aerothermodynamic. 第三，通过数值试验，分析了气体模型和温度模型对热流的影响，对于来流焓值较低的流动，在马赫数较小的情况下，温度升高并不明显，完全气体模型仍然使用，但是对于高焓值以及较大马赫数的流动，温度升高很多，完全气体模型不再适用，必须采用不同的气体模型来代替，本文中采用化学非平衡气体模型。
Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine. 摘要为了使气动热力模型更好的逼近涡轮发动机，应用成熟的非均匀B样条来拟合部件特性。
In accordance with large temperature gradient in multi-stage turbine channel,an aerothermodynamic method is proposed for varying specific heat solution of S 2 surface to consider precisely the effect of temperature variation on the computed results. 针对在多级涡轮流道中沿流动方向燃气温度变化较大这一特点，为了准确反映出温度变化对气动热力计算结果的影响，提出了一种考虑变比热影响的S2流面的气动热力计算方法。
Some Aerothermodynamic Aspects of ESA Entry Probes ESA再入探测器的某些空气热动力问题(英文)
n.空气热力学
