3 参考文献
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题名中译：预处理在黏性流动中的应用。
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题名中译：前飞直升机旋翼非定常可压缩黏性流计算的高阶低耗散方法。
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题名中译：面向空气动力学应用的高阶求解器开发。
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题名中译：无黏可压缩流数值求解的半隐式间断 Galerkin 有限元方法。
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题名中译：求解扩散方程间断 Galerkin 离散的 p 多重网格方法的数值评估。
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题名中译：复杂区域黏性流问题的间断 Galerkin 离散。
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题名中译：一类非线性流体力学问题的混合局部间断 Galerkin 方法。
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题名中译：求解声学问题的高效间断 Galerkin 方法。
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题名中译：非结构网格 Euler 方程的 p 多重网格间断 Galerkin 方法。
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题名中译：水平集方程的免数值求积间断 Galerkin 方法。
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题名中译：采用不同数值通量的 Runge–Kutta 间断 Galerkin 方法性能的数值研究。
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题名中译：采用 hp 多重网格方法的高阶间断 Galerkin 方法。
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题名中译：非结构网格上的高阶节点式间断 Galerkin 网格粒子法。
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题名中译：基于时空展开的间断 Galerkin 格式。Ⅰ. 一维无黏可压缩流。
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题名中译：基于时空展开的间断 Galerkin 格式。Ⅱ. 多维黏性流动方程。
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题名中译：有限体积与间断 Galerkin 格式中扩散通量构造的一项研究。
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题名中译：非定常 Euler 方程高阶间断 Galerkin 离散的隐式求解。
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题名中译：采用 WENO 限制器的 Runge–Kutta 间断 Galerkin 方法。Ⅱ. 非结构网格。
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题名中译：非结构网格上采用新型 WENO 限制器的 Runge–Kutta 间断 Galerkin 方法。
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题名中译：二维非结构网格上黏性可压缩流的谱／hp 方法。
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题名中译：采用谱元法对顶盖驱动立方腔流进行大涡模拟。
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题名中译：非结构网格上的谱元方法：比较与近期进展。
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题名中译：格子 Boltzmann 方法中曲线边界的精确处理。
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题名中译：透平机械模拟的格子 Boltzmann 方法。
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题名中译：格子 Boltzmann 方法的统一边界处理。
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题名中译：格子 Boltzmann 方程的多重网格解法。
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题名中译：采用广义坐标格子 Boltzmann 方法模拟翼型绕流。
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题名中译：格子 Boltzmann 方法的基础气动声学能力。
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题名中译：用于气动声学模拟的格子 Boltzmann 方法精度。
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题名中译：格子 Boltzmann 方法的完全匹配层表述。
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题名中译：扑翼空气动力学的格子 Boltzmann 方法。
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题名中译：可压缩热流体的有限差分格子 Boltzmann 方法。
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题名中译：局部加密网格上的格子 Boltzmann 模拟。
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题名中译：采用格子 Boltzmann 方法分析多段翼型的非定常流动。
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题名中译：采用格子 Boltzmann 方法预测供暖、通风与空调系统噪声。
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题名中译：结合有限体积法与格子 Boltzmann 方法的多尺度、多物理化学过程耦合数值方法。
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题名中译：自然对流的格子 Boltzmann—有限体积混合方法。
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题名中译：格子 Boltzmann 求解器与有限差分求解器的比较。
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题名中译：采用格子 Boltzmann 方法在复合多分辨率网格上进行湍流直接模拟与大涡模拟。
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题名中译：曲线坐标系中对流—扩散方程的格子 Boltzmann 方法。
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题名中译：标准格子上不存在 Galilei 不变性三次缺陷的格子 Boltzmann 算法。
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题名中译：插值方法与格子 Boltzmann 网格加密的精度。
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题名中译：模拟流体与运动细长柔性物体相互作用的格子 Boltzmann—浸入边界方法。
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题名中译：加速求解椭圆型方程的多重网格格子 Boltzmann 方法。
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题名中译：面向复杂飞机应用的无网格 Euler／Navier–Stokes 求解算法。
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题名中译：无网格方法系列论文。
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题名中译：可压缩流的构件式—无网格混合方法。
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题名中译：采用局部径向基函数的无黏可压缩流无网格 Euler 求解器。
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题名中译：统一算法框架下多种无网格格式的比较。
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题名中译：用于外挂物分离预测的笛卡尔网格／无网格混合算法。
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题名中译：非结构网格高 Reynolds 数流动计算的数值问题。
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题名中译：混合非结构网格上黏性流有限体积离散的若干问题。
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题名中译：高度拉伸网格上高 Reynolds 数流动的非结构算法。
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题名中译：采用代数多重网格隐式求解预处理 Navier–Stokes 方程。
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题名中译：采用 Runge–Kutta 时间推进格式的有限体积法求解 Euler 方程。
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题名中译：整机无黏跨声速绕流的计算。
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题名中译：关于中心差分格式与迎风格式。
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题名中译：无黏气体动力学方程的通量矢量分裂及其在有限差分法中的应用。
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题名中译：Euler 方程的通量矢量分裂。
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题名中译：一种新的通量分裂格式。
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题名中译：AUSM 的后续发展：AUSM+。
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题名中译：可压缩流的保正格式与激波建模。
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题名中译：含激波可压缩黏性流的一种新高分辨率格式。
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题名中译：可压缩流的一种简单通量分裂格式。
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题名中译：可压缩与不可压缩流的通量分裂格式。
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题名中译：数值计算流体动力学方程间断解的一种差分格式（原文为俄文，另有英译本）。
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题名中译：双曲型守恒律方程组的迎风差分格式。
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题名中译：近似 Riemann 求解器、参数矢量与差分格式。
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题名中译：非结构网格迎风格式的设计与应用。
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题名中译：气体动力学的 Godunov 型方法。
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题名中译：HLL Riemann 求解器中接触间断的恢复。
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题名中译：关于 Riemann 求解器大讨论的一项研究。
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题名中译：采用加权平均通量格式的强激波稳健 HLLC Riemann 求解器。
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题名中译：非结构网格的多维 HLLC Riemann 求解器及其在 Euler 流动与磁流体动力学流动中的应用。
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题名中译：非常简单、无激波鼓包且能分辨边界层的旋转混合 Riemann 求解器。
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题名中译：双曲型守恒律的高分辨率格式。
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题名中译：曲线坐标系中双曲型守恒律的隐式 TVD 格式。
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题名中译：含时多维气体动力学数值分析的离散模型。
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题名中译：迈向真正的多维迎风格式。
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题名中译：可压缩 Euler 方程的真正多维迎风格式与高效多重网格求解器。
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题名中译：二维 Euler 方程的波动分裂格式。
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题名中译：基于 Euler 方程定常特征的守恒迎风残差分配格式。
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题名中译：非结构网格上的隐式迎风残差分配 Euler 和 Navier–Stokes 求解器。
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题名中译：用于黏性流模拟的紧致残差分配格式。
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题名中译：混合非结构网格上定常无黏流问题的超高阶残差分配格式构造。
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题名中译：一致高阶精度的本质无振荡格式，Ⅲ。
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题名中译：二维双曲型方程组的有限体积高阶 ENO 格式。
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题名中译：高阶空间精度方法的实际应用问题。
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题名中译：非结构网格上的 ENO 格式。
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题名中译：非结构网格上的本质无振荡格式：分析与实现。
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题名中译：加权 ENO 格式的高效实现。
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题名中译：基于最小二乘重构的非结构网格高阶 ENO 格式。
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题名中译：采用外推在非结构网格上获得本质无振荡的 Euler 解。
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题名中译：用于非结构网格平均值插值的加权本质无振荡格式。
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题名中译：WENO 格式中负权重的处理技术。
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题名中译：用于高效可压缩湍流直接数值模拟的带宽优化 WENO 格式。
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题名中译：非结构网格上非线性双曲型方程组的免数值求积无振荡有限体积格式。
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题名中译：双曲型守恒律的改进加权本质无振荡格式。
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题名中译：刚性双曲型平衡律的超高阶精度有限体积格式。
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题名中译：双曲型守恒律的高阶加权本质无振荡 WENO-Z 格式。
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题名中译：任意非结构网格上层流、转捩流和湍流的 WENO 格式。
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题名中译：黏性流的高阶解自适应中心本质无振荡（CENO）方法。
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题名中译：前飞直升机旋翼非定常可压缩黏性流计算的高阶低耗散方法。
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题名中译：基于真正多维 HLL Riemann 求解器的非结构三角形网格 Lagrange 型 ADER-WENO 有限体积格式。
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题名中译：改善加权本质无振荡格式的一种新光滑度指标。
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题名中译：平衡真实气体的通量 Jacobian 矩阵与广义 Roe 平均。
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题名中译：平衡气体流动计算：Ⅱ. 守恒律数值表述的分析。
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题名中译：平衡真实气体的广义通量矢量分裂与 Roe 平均。
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题名中译：非平衡流动计算：Ⅰ. 守恒律数值表述的分析。
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题名中译：计算化学非平衡流动的一组强耦合迎风算法。
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题名中译：一般热化学非平衡流动的迎风算法。
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题名中译：具有非平衡化学与振动松弛的流动通量分裂算法。
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题名中译：具有非平衡化学的真实气体无黏通量分裂算法。
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题名中译：Euler 方程最优光顺多级格式的设计。
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题名中译：采用多重网格方法求解 Euler 方程。
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题名中译：计算跨声速流动。
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题名中译：几种隐式光顺方法的比较。
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题名中译：采用多重网格方法计算黏性流。
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题名中译：对流问题的一种新多重网格方法。
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题名中译：采用直接求解器进行黏性流计算。
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题名中译：三维 Euler 方程的直接与迭代算法。
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题名中译：矩阵计算。
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题名中译：可压缩流的 Schwarz 型算法。
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题名中译：边界层。
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题名中译：湍流剪切流的 Reynolds 应力模型综述。
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题名中译：湍流与转捩建模。
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题名中译：流水理论研究。
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题名中译：直线河床中液体的旋涡与湍动流动理论。
[327] Spalart P, Shur M. On the sensitization of turbulence models to rotation and curvature. Aerospace Sci Tech 1997;5:297-302.
题名中译：使湍流模型对旋转和曲率具有响应的方法。
[328] Shur M, Strelets M, Travin A, Spalart P. Turbulence modeling in rotating and curved channels: assessment of the Spalart-Shur correction term. AIAA Paper 98-0325; 1998.
题名中译：旋转与弯曲通道中的湍流建模：Spalart–Shur 修正项的评估。
[329] Shih TH, Zhu J, Liou WW, Chen K-H, Liu N-S, Lumley J. Modeling of turbulent swirling flows. In: Proc. 11th symposium on turbulent shear flows, Grenoble, France; 1997 [also NASA TM-113112; 1997].
题名中译：湍流旋流的建模。
[330] Chen K-H, Liu N-S. Evaluation of a non-linear turbulence model using mixed volume unstructured grids. AIAA Paper 98-0233; 1998.
题名中译：采用混合体积单元非结构网格评估非线性湍流模型。
[331] Abdel Gawad AF, Abdel Latif OE, Ragab SA, Shabaka IM. Turbulent flow and heat transfer in rotating non-circular ducts with nonlinear $ k-\varepsilon $ model. AIAA Paper 98-0326; 1998.
题名中译：采用非线性 k–ε 模型研究旋转非圆截面管道中的湍流与传热。
[332] Baldwin BS, Lomax HJ. Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow. AIAA Paper 78-257; 1978.
题名中译：分离湍流的薄层近似与代数模型。
[333] Spalart P, Allmaras S. A one-equation turbulence model for aerodynamic flows. AIAA Paper 92-0439; 1992.
题名中译：空气动力学流动的单方程湍流模型。
[334] Launder BE, Spalding B. The numerical computation of turbulent flows. Comput Meth Appl Mech Eng 1974;3:269-89.
题名中译：湍流的数值计算。
[335] Wilcox DC. Reassessment of the scale determining equation for advanced turbulence models. AIAA J 1988;26:1299-310.
题名中译：先进湍流模型中尺度确定方程的重新评估。
[336] Bardina JE, Huang PG, Coakley TJ. Turbulence modeling validation, testing, and development. NASA TM-110446; 1997.
题名中译：湍流建模的验证、测试与开发。
[337] McParlin S, Adamczak D. Comparison of turbulence models for the RAE Model 2155 test cases. AIAA Paper 2003-598; 2003.
题名中译：RAE 2155 模型测试算例的湍流模型比较。
[338] Jameson A. A non-oscillatory shock capturing scheme using flux limited dissipation. MAE Report No. 1653, Dept. of Mechanical and Aerospace Engineering, Princeton University; 1984.
题名中译：采用通量限制耗散的无振荡激波捕捉格式。
[339] Whitfield DL, Janus JM. Three-dimensional unsteady Euler equations solution using flux vector splitting. AIAA Paper 84-1552; 1984.
题名中译：采用通量矢量分裂求解三维非定常 Euler 方程。
[340] Thomas JL, Salas MD. Far field boundary conditions for transonic lifting solutions to the Euler equations. AIAA J 1986;24:1074-80.
题名中译：Euler 方程跨声速升力解的远场边界条件。
[341] Usab WJ, Murman EM. Embedded mesh solution of the Euler equations using a multiple-grid method. AIAA Paper 83-1946; 1983.
题名中译：采用多网格方法的 Euler 方程嵌入网格解法。
[342] Radespiel R. A cell-vertex multigrid method for the Navier-Stokes equations. NASA TM-101557; 1989.
[343] Kroll N, Jain RK. Solution of two-dimensional Euler equations – experience with a finite volume code. DFVLR-FB 87-41; 1987.
题名中译：二维 Euler 方程的求解——有限体积程序的使用经验。
[344] Verhoff A. Modeling of computational and solid surface boundary conditions for fluid dynamics calculations. AIAA Paper 85-1496; 1985.
题名中译：流体动力学计算中计算域边界条件与固体表面边界条件的建模。
[345] Hirsch C, Verhoff A. Far field numerical boundary conditions for internal and cascade flow computations. AIAA Paper 89-1943; 1989.
题名中译：内流与叶栅流计算的远场数值边界条件。
[346] Giles MB. Non-reflecting boundary conditions for Euler equation calculations. AIAA Paper 89-1942; 1989.
题名中译：Euler 方程计算的无反射边界条件。
[347] Tan Z, Wang DM, Srinivasan K, Pzekwas A, Sun R. Numerical simulation of coupled radiation and convection from complex geometries. AIAA Paper 98-2677; 1998.
题名中译：复杂几何中辐射与对流耦合的数值模拟。
[348] Agarwal RK, Schulte P. A new computational algorithm for the solution of radiation heat transfer problems. AIAA Paper 98-2836; 1998.
题名中译：求解辐射传热问题的一种新计算算法。
[349] Hino T. An unstructured grid method for incompressible viscous flows with a free surface. AIAA Paper 97-0862; 1997.
题名中译：具有自由表面的不可压缩黏性流非结构网格方法。
[350] Löhner R, Yang C, Onate E, Idelsson S. An unstructured grid-based, parallel free surface solver. AIAA Paper 97-1830; 1997.
题名中译：基于非结构网格的并行自由表面求解器。
[351] Cowles G, Martinelli L. A cell-centered parallel multiblock method for viscous incompressible flows with a free surface. AIAA Paper 97-1865; 1997.
题名中译：具有自由表面的黏性不可压缩流单元中心并行多块方法。
[352] Wagner CA, Davis DW, Slimon SA, Holligsworth TA. Computation of free surface flows using a hybrid multiblock/chimera approach. AIAA Paper 98-0228; 1998.
题名中译：采用多块／Chimera 混合方法计算自由表面流动。
[353] Calderer A, Kang S, Sotiropoulos F. Level set immersed boundary method for coupled simulation of air/water interaction with complex floating structures. J Comput Phys 2014;277:201-27.
题名中译：采用水平集浸入边界方法耦合模拟空气／水与复杂浮体结构的相互作用。