The effectiveness of delta-wing missile leading-edge control surfaces, one hinged about its rear, the other hinged about its midlength point was studied. A scale model of the missile was tested in a 7 x 5 ft wind tunnel, at a Mach Number of 0.12 and a Reynolds number of ...
2) flap control 后缘附翼控制3) frontier and rear 前缘与后缘 例句>> 4) leading-edge and trail-edge 前后缘 1. Design and application of straight leading-edge and trail-edge technology for wind turbine blades; 风力机叶片的分段直前后缘设计技术与应用 更多例句>> ...
aleading edge lip deflection, and leading edge blunting via compliant surfaces actuated with SMAs. 前进嘴唇偏折和前进钝通过服从的表面开动与SMAs。 [translate] akarl pearson 卡尔pearson [translate] atake a [oa] 作为 [translate] aIt is not Kelsey's computer game 它不是Kelsey的计算机游戏 [...
leading edge - forward edge of an airfoil aerofoil, airfoil, control surface, surface - a device that provides reactive force when in motion relative to the surrounding air; can lift or control a plane in flight edge - a sharp side formed by the intersection of two surfaces of an object...
aImportant core technology efforts addressed needs for quasi-static shape control for inlet shaping, 重要对quasi-static成形控制的核心技术努力被处理的需要为入口塑造, [translate] aleading edge lip deflection, and leading edge blunting via compliant surfaces actuated with SMAs. 前进嘴唇偏折和前进钝通过...
A system for controlling a high-lift device of an aircraft may include an interface for placement in a flight deck of an aircraft. The interface may include an edge control device f
As a control surface, plain flap surfaces with the hingeline at the center of the circle are difficult to mass balance and require the addition of structural arms to carry a block of mass balance. Also, a plain flap with large overhangs result in a large movement of its leading edge up ...
The invention relates to a wing leading-edge device, a wing having a fixed wing body and a wing leading-edge device, as well as an aircraft. BACKGROUND OF THE INVENTION In commercial aircraft, the icing of wing components and control surfaces is often prevented by using deicing or anti-ic...
This winglet promotes sonic boom minimization. Further, the wing tip anhedral allows greater inboard dihedral. This effectively pushes lift aft for sonic boom and control purposes while minimizing the movement of control surfaces. 展开 收藏 引用 批量引用 报错 分享 ...
12. With turbine blades rotate to the last two stages, the pressure differentiations between the suction and pressure surfaces are observed to be diminished further, which are quite similar to the results of approximate torques generated from the baseline and the improved models in the range ...