| 1. | Nonlinear turbulence models in shock boundary - layer interaction
边界层相互作用的非线性湍流模式 |
| 2. | Numerical simulation of two - dimensional shock boundary - layer interaction between a rocket and booster
助推器附近二维激波边界层干扰的数值分析 |
| 3. | The computed results compared favorably with measurements and the corresponding shock boundary - layer interaction and energy loose during transonic speed was described
以寻找出叶片对能量转换过程中，因气动力原因而造成能量损失的原因，进而提供改良建议。 |
| 4. | In this study , the transonic shock - wave / boundary - layer interaction and viscous shear stress for the turbine and compressor stator were simulated used the implicit two - factor flux - splitting schemes for solving the thin - layer compressible flow
除验证各式正确性外并仿真叶片外形对气流分离、震波/边界层相互干扰及压缩比等关系，以及流体黏滞性等影响下，引擎能量损失与效益分析。 |
| 5. | In this study , the transonic shock - wave / boundary - layer interaction and viscous shear stress for the turbine and compressor stator were simulated used the implicit two - factor flux - splitting schemes for solving the thin - layer compressible flow
除验证各式正确性外并模拟叶片外形对气流分离、震波/边界层相互干扰及压缩比等关系，以及流体黏滞性等影响下，引擎能量损失与效益分析。 |
