| 1. | Empirical results are needed in the transonic mach regime .
在跨音速马赫数范围内需要经验结果。 |
| 2. | Unlike in subsonic and transonic speed regimes, the interference resulting from the finite size of the test region is seldom present .
不像在亚、跨音速区域，这里因试验段尺寸有限造成的干扰是难得存在的。 |
| 3. | Analysis study on transonic speed equal amplitude vibration of a certain type of aircraft
某型机跨音速等幅振动研究 |
| 4. | The effect of turbine blade positive curving on the flow field of a turbine transonic cascade
叶片弯曲对跨音速涡轮叶栅流场的影响 |
| 5. | Abstract : an effective aerodynamic optimization design method of transonic airfoil is given
文摘:提出了一种有效的跨音速翼型气动优化设计方法。 |
| 6. | Computation of wing flutter for unsteady transonic flows in the frequency domain is studied in this thesis
本文研究了机翼跨音速颤振的频域计算方法。 |
| 7. | Numerical simulation of full three - dimensional viscous flow field in a multi - stage transonic gas turbine
某双级跨音速燃气透平全三元粘性流场的数值分析 |
| 8. | An integral boundary layer method based on the dissipation integral is used to account for viscous effects
考虑附面层影响，通过粘/位迭代得到跨音速翼/体的非定常气动力。 |
| 9. | Investigation on the gas flow field with viscous , active , stride - sonic , compressible for high voltage sfs circuit breaker
高精度有粘、可压缩、有源、跨音速气流场求解的研究。 |
| 10. | Numerical results show that the method provides an effective tool for refining and designing a fransonic airfoil
算例结果表明，本方法提供了一种跨音速翼型改型设计及新翼型设计的有效工具。 |
