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標(biāo)題: Titlebook: Smart Intelligent Aircraft Structures (SARISTU); Proceedings of the F Piet Christof W?lcken,Michael Papadopoulos Conference proceedings 201 [打印本頁]

作者: 贊美    時間: 2025-3-21 17:45
書目名稱Smart Intelligent Aircraft Structures (SARISTU)影響因子(影響力)




書目名稱Smart Intelligent Aircraft Structures (SARISTU)影響因子(影響力)學(xué)科排名




書目名稱Smart Intelligent Aircraft Structures (SARISTU)網(wǎng)絡(luò)公開度




書目名稱Smart Intelligent Aircraft Structures (SARISTU)網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Smart Intelligent Aircraft Structures (SARISTU)被引頻次




書目名稱Smart Intelligent Aircraft Structures (SARISTU)被引頻次學(xué)科排名




書目名稱Smart Intelligent Aircraft Structures (SARISTU)年度引用




書目名稱Smart Intelligent Aircraft Structures (SARISTU)年度引用學(xué)科排名




書目名稱Smart Intelligent Aircraft Structures (SARISTU)讀者反饋




書目名稱Smart Intelligent Aircraft Structures (SARISTU)讀者反饋學(xué)科排名





作者: 雕鏤    時間: 2025-3-21 23:23
Influence of ,, and , Criteria on Feed-Forward Gust Loads Control Optimized for the Minimization of aneuver and gust loads. It is shown that the choice of the cost function has a significant influence on this optimum and the resulting wing box mass. Both .. and . criteria are investigated. Based on the optimization results, a potential total wing box mass saving is proposed for further aircraft performance assessment.
作者: 蛙鳴聲    時間: 2025-3-22 02:07

作者: 使長胖    時間: 2025-3-22 05:00
Seamless Morphing Concepts for Smart Aircraft Wing TipA variety of material samples and joints were prepared and tested in order to provide a database for numerical simulation and sizing. One of the proposed solutions was developed until the physical sub-component level. Finally, morphing parts were prepared and delivered for assembly in ground test and true-scale wind tunnel demonstrators.
作者: Cpap155    時間: 2025-3-22 11:36
Conference proceedings 2016d at Moscow, Russia between 19-21 of May 2015. The SARISTU project, which was launched in September 2011, developed and tested a variety of individual applications as well as their combinations..With a strong focus on actual physical integration and subsequent material and structural testing, SARIST
作者: 外形    時間: 2025-3-22 16:26

作者: 有害處    時間: 2025-3-22 18:54

作者: 激勵    時間: 2025-3-22 21:49

作者: 上漲    時間: 2025-3-23 03:39

作者: AGOG    時間: 2025-3-23 06:09

作者: 咆哮    時間: 2025-3-23 10:23

作者: profligate    時間: 2025-3-23 14:45
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
作者: euphoria    時間: 2025-3-23 19:12

作者: Obstruction    時間: 2025-3-23 23:51

作者: restrain    時間: 2025-3-24 05:05
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
作者: BRIDE    時間: 2025-3-24 09:45

作者: 雕鏤    時間: 2025-3-24 12:00
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
作者: Adulate    時間: 2025-3-24 17:07
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.
作者: 省略    時間: 2025-3-24 21:39
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
作者: 漂亮    時間: 2025-3-25 02:36

作者: 破裂    時間: 2025-3-25 05:26

作者: 皺痕    時間: 2025-3-25 10:49
Dynamic Aircraft Model with Active Winglet, Effects of Flight Mechanics and Loads Analysiss in application scenario AS03. The models have been developed from the initial SARISTU wing model of Alenia Aermacchi (AAM). A mass model of the fuel has been reconstructed from the aircraft data, and an aircraft model has been developed using an aircraft sizing tool. With the completion of the win
作者: 虛假    時間: 2025-3-25 13:28

作者: Anguish    時間: 2025-3-25 18:44
rphing aerodynamic surface, and practical nanocomposite adva.The book includes the research papers presented in the final conference of the EU funded SARISTU (Smart Intelligent Aircraft Structures) project, held at Moscow, Russia between 19-21 of May 2015. The SARISTU project, which was launched in
作者: 亞當(dāng)心理陰影    時間: 2025-3-25 23:05

作者: Wordlist    時間: 2025-3-26 03:07
Olaf Heintze,Stefan Steeger,Alexander Falken,Jürgen Heckmann
作者: hysterectomy    時間: 2025-3-26 05:01
Markus Kintscher,Johannes Kirn,Stefan Storm,Fabian Peter
作者: NOVA    時間: 2025-3-26 11:17

作者: PRO    時間: 2025-3-26 16:29

作者: flavonoids    時間: 2025-3-26 20:50

作者: CUMB    時間: 2025-3-26 23:57
Yasser Essa,Federico Martin de la Escalera Cutillas,Ignazio Dimino,Monica Ciminello,Antonio Concilio
作者: Flavouring    時間: 2025-3-27 02:27

作者: 手術(shù)刀    時間: 2025-3-27 08:08

作者: Presbyopia    時間: 2025-3-27 11:33
Christof Nagel,Arne Fiedler,Oliver Schorsch,Andreas Lühring
作者: ANA    時間: 2025-3-27 17:24

作者: savage    時間: 2025-3-27 18:46
Charles Charyeration experiments at the Daresbury Laboratory. To achieve even higher longitudinally polarised terahertz electric field strengths, and to be able to temporally tune the terahertz radiation, the author investigated generation within non-linear optical crystals. He developed a novel generation schem
作者: Brocas-Area    時間: 2025-3-28 01:37
Vladimir Snop,Vaclav Horakeration experiments at the Daresbury Laboratory. To achieve even higher longitudinally polarised terahertz electric field strengths, and to be able to temporally tune the terahertz radiation, the author investigated generation within non-linear optical crystals. He developed a novel generation schem
作者: 朦朧    時間: 2025-3-28 05:29

作者: 多余    時間: 2025-3-28 09:10

作者: 珍奇    時間: 2025-3-28 14:10

作者: blight    時間: 2025-3-28 16:44
Development and Validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose. Three specimens were assembled and subjected to bird impact tests. Two of those specimens were used to compare the behaviour and the efficiency of the splitter and the absorber at “iso-mass” solutions. The third and fourth tests were performed on a representative EADN leading edge structure connec
作者: GNAW    時間: 2025-3-28 21:26

作者: 作嘔    時間: 2025-3-28 23:04

作者: GRAIN    時間: 2025-3-29 05:21

作者: 轎車    時間: 2025-3-29 08:13

作者: 聲音刺耳    時間: 2025-3-29 15:08

作者: Glycogen    時間: 2025-3-29 19:28
Dynamic Aircraft Model with Active Winglet, Effects of Flight Mechanics and Loads Analysisployed in the design of GLAS and WATE controller optimization and investigations to verify possible wing structure mass reductions. The approach and dynamic loads models developed in SARISTU can be applied straightforward in future R&D projects for structure loads assessments (aeromechanical), contr
作者: 流動才波動    時間: 2025-3-29 23:11

作者: 絕緣    時間: 2025-3-30 01:50

作者: 災(zāi)難    時間: 2025-3-30 06:28

作者: Gastric    時間: 2025-3-30 09:25

作者: Cocker    時間: 2025-3-30 14:31

作者: BUCK    時間: 2025-3-30 16:34
978-3-319-37010-1Springer International Publishing Switzerland 2016
作者: 受辱    時間: 2025-3-31 00:28

作者: drusen    時間: 2025-3-31 04:04
https://doi.org/10.1007/978-3-319-22413-8Multifunction Materials; Multifunctional Structures; Nanocomposite Manufacturing; SARISTU; Smart Intelli
作者: 無王時期,    時間: 2025-3-31 08:45

作者: Mutter    時間: 2025-3-31 11:20
Winglet Design, Manufacturing, and Testing3 has been developed. Full-scale demonstrator has been manufactured and successfully tested to prove the maturity of such a device and its technology. This paper contributes to the overview of design, manufacturing, and testing aspects of WATE demonstrator.
作者: finale    時間: 2025-3-31 16:03

作者: neurologist    時間: 2025-3-31 18:42

作者: 流利圓滑    時間: 2025-4-1 00:56
Lothar Volkeltews the complex history of the glucose-sensing machinery in .Since the 1970s, there has been much discussion about the “glucoreceptor” and?“substrate site” and which of these two is the dominant theory, but new findings on the glucose-sensing receptor have now shed new light on the “glucoreceptor th
作者: 場所    時間: 2025-4-1 02:55
1431-875X to a number of standard results, with many proofs.Solutions This graduate-level textbook is primarily aimed at graduate students of statistics, mathematics, science, and engineering who have had an undergraduate course in statistics, an upper division course in analysis, and some acquaintance with m
作者: capsule    時間: 2025-4-1 07:52





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