swept wing

Full 3D iterative solution of transonic flow for a swept wing test channel

后掠冀跨声流场S1/S2流面全三元迭代解

The flow over delta wing with 65 ° and 70 ° swept at high angle of attack is investigated by solving the three dimensional, compressible Navier Stokes equations utilizing the second order upwind TVD algorithm ( Harten Yee).

采用Harten－Yee的二阶精度隐式TVD格式对N－S方程进行数值模拟，研究了后掠角为65°和70°的三角翼绕流的流场特性。

Flow Control Technique for Forward-swept Wing Blended Body Tailless Configuration

前掠翼融合体无尾布局流动控制技术

This paper investigates a new flow control technique based on a forward-swept wing blended body ( FBB) tailless configuration by a wind tunnel.

通过风洞实验，研究了基于前掠翼融合体无尾气动布局的一种新概念流动控制技术。

On a swept wing airplane, this effect is due to two causes.

在后掠翼飞机, 这种效果是由于两个原因.

The H-O grid is suggested in this paper to compute the compressible flow past highly swept slender wing-body combinations. Full-potential equation, finite difference method and approximate factorization iteration scheme are used.

用H－O网格、守恒型全位势方程、差分和隐式近似因式分解迭代算法计算绕大后掠细长翼－身组合体的可压缩流动。

A variant of the swept-back wing is the delta wing.

后掠翼的变型是三角翼.