试飞结果表明，机翼蒙皮直接改装测量孔和测压带方法均能有效测量机翼表面压力分布。
The flight test results show that the Stripe-A-Tube method is as more effective as measurement that transform hole of static pressure on wing surface.
试飞结果表明，机翼蒙皮直接改装测量孔和测压带方法均能有效测量机翼表面压力分布。
The flight test results show that the Stripe-A-Tube method is as more effective as measurement that transform hole of sta…
论文以大展弦比飞翼布局机翼蒙皮的优化设计为背景，开展了复合材料层压板结构的优化设计工作。
In this paper, an effective design optimization method for High-aspect-ratio composite wing skin is presented.
整体油箱，由机翼结构件梁、肋、蒙皮组成，用来在飞机上储存燃油的金属容器。
INTEGRAL TANK, a metal container formed by the wing structure (spars, ribs, skin) for storage of fuel on the airplane.
例如，可以使用接头将强化板、悬浮翼脚或纵梁接合到诸如机翼或机身蒙皮之类的面板。
For instance the joint may be used to join a reinforcing plate, floating rib foot, or stringer to a panel such as a wing or fuselage cover.
机翼的蒙皮要有足够大的面内伸缩变形能力，同时还要有足够的面外承载能力。
The flexible skins must have substantial in-plane expansion deformability, while at the same time it must be able to bear the out-of-plane aerodynamic loads.
次要结构由机翼前缘，后缘和翼尖构成，主要用来减小空气阻力，支撑蒙皮，协助飞行操纵面和操纵机构。
The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.
复合材料蒙皮稳定性是飞机翼面结构设计需要考虑的重要方面。
Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures.
复合材料蒙皮稳定性是飞机翼面结构设计需要考虑的重要方面。
Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures.
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