2017年8月6日 · Wing in bending (positive load factor) loads the upper skins in compression and lower skins in tension. A collapse moment analysis examines the interaction between the wing …

The skin of an aircraft is the outer surface which covers much of its wings and fuselage. The most commonly used materials are aluminum and aluminium alloys with other metals, including …

2024年6月1日 · By using polymeric skin, engineers can design wings that can morph to meet the specific requirements of each flight, which results in improved performance and increased …

2023年1月18日 · This paper demonstrates a stacking sequence optimisation process of a composite aircraft wing skin. A two-stage approach is employed to satisfy all sizing …

Wing Skin. Often, the skin on a wing is designed to carry part of the flight and ground loads in combination with the spars and ribs. This is known as a stressed-skin design. The all-metal, …

22.16.2.3. Wing Skin. Often, the skin on a wing is designed to carry part of the flight and ground loads in combination with the spars and ribs. This is known as a stressed-skin design. The all …

2022年9月1日 · Polymeric skins need more actuation force in the slower direction when deform biaxially. Silicone based Ecoflex shows least stiffness and hysteresis loss. There is an …

2021年9月13日 · This paper presents a parametric study of a composite skin for a twist-morphing wing. The skin is made of periodic laminated composite sections, called “Twistkins”, integrated …

2022年9月6日 · We proposed a laminate parameter-based optimization strategy that considers the stiffness characteristics of the two-dimensional elements used as design variables.

2019年3月19日 · In this paper, a new concept of a gripper pin structure is proposed for an aircraft morphing wing that can decouple in-plane stiffness from out-of-plane stiffness. There has been …