读音:美英 double wedge airfoil基本解释 双楔翼形 分词解释 double双的 wedge楔 airfoil机翼,螺旋桨 double wedge airfoil是什么意思 double wedge airfoil怎么读 double wedge airfoil在线翻译 double wedge airfoil中文意思 double wedge airfoil的解释 double wedge airfoil的发音 double wedge airfoil意思是什么 double...
网络释义 1. 双楔翼剖面 wedge - 楔 ... 视差测高楔 parallax wedge双楔翼剖面double-wedge airfoil调整楔 adjusting wedge ... terms.naer.edu.tw|基于4个网页
2) flattened double-wedge profile 前后缘楔形平翼(火)3) biconvex wing ; biconvex airfoil; double-cambered wing 双凸形机翼4) wedge-shaped airfoil 楔形翼切面5) crossed wing 十字形机翼(火)6) double-delta wing 双三角形机翼补充资料:鳞石英楔形双晶 鳞石英楔形双晶 鳞石英楔形双晶 说明:补充...
Flow Visualization around a Double Wedge Airfoil Model with Focusing Schlieren System 振动波纹影法跨音速流双重楔机翼模型在现在的学习,双楔机翼模型的空气动力学的特征被把吃惊试管用作一条断断续续的风隧道在接近音速的流动调查.司机和吃惊试管的驾驶气体是干燥空气.两倍楔的机翼模型有 58 公里的跨度, 75 公里...
Aerodynamic analysis is part of the whole procedure, which includes focusing on airfoil shapes which will permit sustained flight of aircraft at these speeds. Airfoil shapes differ based on the applications, hence the airfoil shapes considered for supersonic speeds are different from the ones ...
3) modified double wedge airfoil 双菱形翼型4) double-wedge wing 菱形翼型机翼5) rhombic sections 菱形截面 1. Load-deformation relationship curves of steel tube beam columns with rhombic sections are calculated by the ABAQUS software,and the calculated main parameters are steel yield strength and...
Double Wedge AirfoilSchlieren MethodCompressible FlowShock TubeIn the recently, it was showed that the airfoil model constructed with flat panels (based on double wedge airfoil) had the flight ability in the subsonic and transonic conditions. However there are few experimental aerodynamic data on the...
The apex of the double wedge airfoil model is located on the 35% chord length from the leading edge. The range of hot gas Mach numbers are from 0.80 to 0.88, and the Reynolds numbers based on chord length are 3.11 脳 10 5 3.49 脳 10 5 , respectively. The flow visualizations were ...
The aerodynamic characteristics namely; lift and drag are analysed by numerically solving compressible Navier-Stokes equations in the flow field around double wedge airfoil by parameterising the angle of attack 伪 and thicknessV. GopalR. Kolluru...
A unified supersonic/hypersonic theory is given of flow past a pitching oscillating double wedge airfoil at arbitrary mean angle of attack. The amplitude and the (reduced) frequency parameter of the oscillation are assumed small and a perturbation method is employed. Closed form formulae are ...