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1·L. Crocco. One-Dimensional Treatment of Steady Gas Dynamics.

克罗柯。定常气体动力学的一维处理法。

2·Three face into the wind design, reasonable space Gas dynamics, low energy efficiency.

三面进风设计，合理的空气动力学，低能耗净化效率。

3·The relationship between the non-equilibrium phenomena and rarefied gas dynamics is discussed.

讨论了非平衡现象与稀薄气体动力学的关系。

4·It is a kernel in the ratified gas dynamics to solve the flow problem in the transitional domain.

求解过渡领域的流动问题，是稀薄气体动力学的核心内容。

5·The flight of space vehicles, probes and shuttles set new demand on gas dynamics, including rarefied gas dynamics.

飞船、宇航探测器、航天飞机等复杂外形航天器给气体动力学，包括稀薄气体动力学提出了新的要求。

6·References 1, 2, and 10 give discussion of the extensions to classical one-dimensional gas dynamics that we will discuss.

参考文献1、2和10对其后我们将讨论的经典一维空气动力学的扩展作了讨论。

7·The equivalence principle of solutions of nonlinear large gas dynamics waves and of solutions of water wave equations will be used.

非线性的大的气体动力学波和水波方程式的溶液的解决办法的相等原则将被使用。

8·Numerical results of two-dimensional Euler equations of compressible gas dynamics verify the accuracy and robustness of the method.

通过计算二维可压缩流欧拉方程组的几个算例，数值结果表明，该格式具有高精度、高分辨率及计算简单的特点。

9·The existence and producing conditions of non-isoentropy flow and non-isoentropy wave have been argumented in classical gas dynamics.

在经典气动力学中讨论了非等熵流和非等熵波的存在和产生的条件。

10·The models of the spinning induced effects upon propellant grain stress and deformation, thermodynamics and gas dynamics were set up.

给出了旋转对推进剂应力应变的影响、产生的热力学方面的影响及旋转引起的气体动力学的影响等的分析计算模型。