翼表面 meaning in Chinese
wing surface
Examples
- If this load centroid is behind the elastic axis of the wing structure, then a nose-down twist of the main wing surface results .
如果该载荷重心在机翼结构弹性轴之后，则引起主机翼表面前端向下的扭转。 - At last , the effect on the outer ballistic trajectory characteristic after the ablation of hypersonic projectile wing has been analyzed
最后，初步分析了高超声速弹翼表面发生烧蚀后对其外弹道特性的影响。 - The interior temperature distribution and ablation model of projectile wing is established from general transmitting heat differential equation ; at the same time , the heat flow density and pressure distribution model of projectile wing is also established
从一般形式的导热微分方程出发，逐步建立了弹翼内部温度分布和烧蚀的数学计算模型；与此同时，建立了弹翼表面的热流密度和压力分布的数学模型。 - In order to predict hydrodynamic characteristics a computational system is developed including determination of the pressure distribution on a wing section by use of the conformal mapping method and panel method respectively and of the flow in boundary layer according to the thin shear layer approximation ( tsl ) for navier - stokes equation approach . the wing sections of naca4412 and naca0012 are applied to test the computational system . the numerical inspection shows that the panel method with better precision and the momentum and the displacement thickness of boundary layer can be used to complete this calculation
本文分别用守屋的保角变换法和基于源汇涡分布的面元法，建立了计算桨叶表面压力分布的数学模型；应用纳维-斯托克方程的薄层近似理论模式和有限差分数值方法，建立了计算机翼表面边界层内部流动的数学模型；应用桨叶表面边界层内部粘性流动和外部势流流动在边界上的匹配算法，建立了桨叶表面二相流流动的计算方法和相应的计算机程序。