咆哮 发表于 2025-3-23 10:23:33
http://reply.papertrans.cn/87/8689/868841/868841_11.pngprofligate 发表于 2025-3-23 14:45:19
Enhanced Adaptive Droop Nose—from Computer Model to Multi-functional Integrated Partmposite gapless and flexible droop nose (enhanced adaptive droop nose, EADN) on the basis of computer models and in compliance with standards and requirements of industrial integration. Therefore, various individual disciplines are integrated into one single manufacturing process and, thus, into oneeuphoria 发表于 2025-3-23 19:12:46
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http://reply.papertrans.cn/87/8689/868841/868841_14.pngrestrain 发表于 2025-3-24 05:05:48
Structural Design of an Adaptive Wing Trailing Edge for Large Aeroplanesentation of the architecture on large aeroplanes. Fast and reliable elementary methods combined with rational design criteria were adopted in order to preliminarily define ATED box geometry, structural properties, and the general configuration of the embedded mechanisms enabling box morphing under tBRIDE 发表于 2025-3-24 09:45:34
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Elastomer-Based Skin for Seamless Morphing of Adaptive Wingsptimize fatigue and ageing properties of this new multi-material device, FEM simulations and mechanical tests are carried out. Two large skin panels are finally manufactured and successfully assembled into a true-scale wind tunnel demonstrator for the experimental validation of adaptive trailing edgAdulate 发表于 2025-3-24 17:07:31
Manufacturing and Testing of Smart Morphing SARISTU Trailing Edgeg technology for future and next-generation aircrafts. Morphing aircraft changes its external geometry significantly during flight which moderates the design requirements. Adaptive Trailing Edge Device (ATED) is designed and manufactured under SARISTU (Smart Intelligent Aircraft Structures) project.省略 发表于 2025-3-24 21:39:25
Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edgended to improve the aircraft’s efficiency aerodynamically, but simultaneously they introduce important loads into the main wing structure. These additional loads lead to heavier wing structure and can thus diminish the initial benefit. Preliminary investigations have shown that a wingtip active trai漂亮 发表于 2025-3-25 02:36:49
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