A simple nonlinear wing theory for the low-aspect-ratio rectangular flat plate with large angle of attack in incompressible flow is developed. 本文系对不可压缩流体中大冲角小展弦比矩形平板机翼提出&个简单的非线性理论。
Experimental study on the behavior of three-dimensional turbulent boundary layer induced by a straight wing erected on a flat plate 对安放直机翼的平板测定三维湍流边界层的低、亚音速特性
The behavior of three-dimensional turbulent boundary layer in the attached flow region induced by a straight wing erected on a flat plate at low and subsonic speeds has been determined experimentally. 本文介绍了在低速和亚音速来流情况下,对一安放着直机翼的平板,在其附体流部分所作的三维湍流边界层特性的测量;