| 1. | The wake survey cannot be used to measure the drag of stalled airfoil or of airfoils with flaps down .
尾流测量不能用来测量失连状态下的冀型或襟翼偏转后的翼型阻力。
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| 2. | As design studies progressed it was found that several airfoil shapes could be used to satisfy the new performance criteria .
当进行设计的研究工作后，发现有几种翼型可以用来满足新的性能指标。
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| 3. | Computation of glaze ice accretion on airfoil
考虑传质传热效应的翼型积冰计算
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| 4. | Numerical simulation of ice accretion on airfoils
飞机机翼结冰过程的数值模拟
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| 5. | The tutorial begins with a simple four - segment airfoil
补习始于一个简单的四部分机翼
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| 6. | A somewhat improved method for analyzing multi - element airfoils
多段翼型的一种分析方法
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| 7. | Numerically simulating of ice accretion on airfoil
翼型积冰的数值模拟
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| 8. | Simulation of flow around an airfoil by the lattice boltzmann method
方法的翼型绕流数值模拟
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| 9. | Multi - objective optimization of airfoils
翼型多目标气动优化设计方法
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| 10. | Numerical analysis of low - reynolds - number flow over airfoil
绕翼型低雷诺数流动的数值分析研究
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