该文应用低阶速度势面元法建立了预报三维水翼水动力性能的数值方法，重点对翼梢和尾涡进行了研究。
A potential-based surface panel method is applied to predicting the performance for three-dimensional hydrofoils, with emphasis on the tip region.
本文将对二元翼型及三角翼等内部声激励的应用研究提供有价值的实验结果。
This paper provides valuable experimental results for the applied study of internal acoustic exc...
本文将对二元翼型及三角翼等内部声激励的应用研究提供有价值的实验结果。
This paper provides valuable experimental results for the applied study of internal acoustic excitation of a two-dime…
本文将对二元翼型及三角翼等内部声激励的应用研究提供有价值的实验结果。
This paper provides valuable experimental results for the applied study of internal acoustic excitation of a two-dimensional airfoil or a delta wing.
本文应用三元亚音速升力面理论求出了后掠翼前缘附近的流场。
The unsteady flow field near the leading edge of an oscillating sweptback wing is obtained by using 3-D subsonic lifting surface theory.
本文应用三元亚音速升力面理论求出了后掠翼前缘附近的流场。
The unsteady flow field near the leading edge of an oscillating sweptback wing is obtained by using 3-D subsonic lifting surface theory.
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