后掠机翼

中等后掠机翼平面参数设计与实验研究

Design and Wind Tunnel Experimental Investigation of Middling Sweepback Wing Plane Parameter

无限翼展后掠机翼的三元湍流边界层计算

Calculation of three-dimensional turbulent boundary layer on an infinite swept wing

变后掠机翼电液伺服加载系统的智能控制

Intelligent control of electrohydraulic servo loading system for variable-sweep aircraft wing

后掠机翼跨音速绕流的二级近似方法

Second order approximation method for transonic flows over swept wings

后掠机翼尾涡面和下洗场计算

Calculation of Trailing Vortex Sheet and Downwash Field Behind a Sweptback Wing

后掠机翼的前缘吸力

On the unsteady leading edge suction of a sweptback wing

（飞行器）有后掠机翼的。

( of an aircraft ) having sweptback wings .

大后掠机翼翼尖导弹动力响应空测与数据分析

Air surveying and data analysis for dynamic response of missiles at swept-back wing tip

后掠机翼低速流动转捩位置的升华法测量

Measurement of Transition Location Change of Swept Wing in a Low-Speed Flow Based on Sublimation Method

采用可压缩线化稳定性理论对后掠机翼的层流边界层稳定性进行了计算研究。

The boundary layer stability on swept wings is investigated computationally by using three-dimensional compressible laminar stability theory .

该控制器应用于变后掠机翼的结构强度加载控制系统之中。

This controller is applied to the structural strength loading control system , which is the experimental system of a variable swept aircraft wing .

从三维时间相依可压缩边界层动量积分方程和平均流动能积分方程出发，将二维可压缩层、湍流边界层积分方程算法推广到求解有限翼展后掠机翼的边界层流动。

Based on three-dimensional , time-dependent momentum and mean-flow kinetic energy integral equations for compressible boundary Layers in nonorthogonal curvilinear coordinates , the existing algorithm for two-dimensional , compressible , Laminal and turbulent integral equations is extended to solve the boundary-layer problem over finite swept wings .

后掠型平板机翼模型的实验模态分析

Experimental Modal Analysis on the Swept & Winged Plate Model

耦合三维非定常Navier-Stokes方程与Euler刚体运动方程数值研究80°尖前缘后掠三角翼的机翼摇滚问题。

The unsteady , compressible , full Navier-Stokes ( N-S ) equations and Euler equation of rigid-body dynamics are sequentially solved to simulate the wing rock phenomenon of 80 ° sweep , sharp edged delta wing .