找回密碼
 To register

QQ登錄

只需一步,快速開始

掃一掃,訪問微社區(qū)

打印 上一主題 下一主題

Titlebook: Smart Intelligent Aircraft Structures (SARISTU); Proceedings of the F Piet Christof W?lcken,Michael Papadopoulos Conference proceedings 201

[復制鏈接]
樓主: 贊美
11#
發(fā)表于 2025-3-23 10:23:33 | 只看該作者
12#
發(fā)表于 2025-3-23 14:45:19 | 只看該作者
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 one
13#
發(fā)表于 2025-3-23 19:12:46 | 只看該作者
14#
發(fā)表于 2025-3-23 23:51:07 | 只看該作者
15#
發(fā)表于 2025-3-24 05:05:48 | 只看該作者
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 t
16#
發(fā)表于 2025-3-24 09:45:34 | 只看該作者
17#
發(fā)表于 2025-3-24 12:00:17 | 只看該作者
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 edg
18#
發(fā)表于 2025-3-24 17:07:31 | 只看該作者
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.
19#
發(fā)表于 2025-3-24 21:39:25 | 只看該作者
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
20#
發(fā)表于 2025-3-25 02:36:49 | 只看該作者
 關于派博傳思  派博傳思旗下網站  友情鏈接
派博傳思介紹 公司地理位置 論文服務流程 影響因子官網 吾愛論文網 大講堂 北京大學 Oxford Uni. Harvard Uni.
發(fā)展歷史沿革 期刊點評 投稿經驗總結 SCIENCEGARD IMPACTFACTOR 派博系數 清華大學 Yale Uni. Stanford Uni.
QQ|Archiver|手機版|小黑屋| 派博傳思國際 ( 京公網安備110108008328) GMT+8, 2026-1-27 01:14
Copyright © 2001-2015 派博傳思   京公網安備110108008328 版權所有 All rights reserved
快速回復 返回頂部 返回列表
鄂托克前旗| 东方市| 华蓥市| 县级市| 惠安县| 上饶市| 涿州市| 资溪县| 潢川县| 河间市| 随州市| 来安县| 台南县| 西藏| 育儿| 孟村| 长海县| 塔河县| 尚志市| 石台县| 且末县| 民勤县| 大埔区| 榆林市| 泸水县| 张掖市| 进贤县| 承德县| 甘德县| 五莲县| 吴旗县| 鲁甸县| 承德县| 隆昌县| 大埔区| 开封市| 金华市| 茂名市| 穆棱市| 云霄县| 竹溪县|