標(biāo)題: Titlebook: ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing; Proceedings of the 3 Antoni Niepokolczycki,Jerzy Komorowski Conferen [打印本頁(yè)] 作者: 閃爍 時(shí)間: 2025-3-21 20:06
書目名稱ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing影響因子(影響力)
書目名稱ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing影響因子(影響力)學(xué)科排名
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書目名稱ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing被引頻次學(xué)科排名
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書目名稱ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing年度引用學(xué)科排名
書目名稱ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing讀者反饋
書目名稱ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing讀者反饋學(xué)科排名
作者: 粗魯性質(zhì) 時(shí)間: 2025-3-21 20:34
Lecture Notes in Mechanical Engineeringhttp://image.papertrans.cn/i/image/460074.jpg作者: 暗諷 時(shí)間: 2025-3-22 01:56 作者: cognizant 時(shí)間: 2025-3-22 08:07 作者: 徹底明白 時(shí)間: 2025-3-22 09:23
ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing978-3-030-21503-3Series ISSN 2195-4356 Series E-ISSN 2195-4364 作者: GEM 時(shí)間: 2025-3-22 15:06 作者: 無(wú)意 時(shí)間: 2025-3-22 20:34
Hiroshi Kuroki,Yukihiro Kondo,Tsukasa Wakabayashi,Kenji Nakamura,Kikuo Takamatsu,Koji Nezaki,Mitsuyoestitution...In this work, young people interviewed over a span of seven years reflect, in real time, on the intended and unintended consequences boarding has had in their own lives. They relate expected and dr978-981-16-6011-5978-981-16-6009-2Series ISSN 2524-5767 Series E-ISSN 2524-5775 作者: ABASH 時(shí)間: 2025-3-23 00:57
Xiang Zhang,Abdul Khadar Syed,Romali Biswal,Filomeno Martina,Jialuo Ding,Stewart Williamsestitution...In this work, young people interviewed over a span of seven years reflect, in real time, on the intended and unintended consequences boarding has had in their own lives. They relate expected and dr978-981-16-6011-5978-981-16-6009-2Series ISSN 2524-5767 Series E-ISSN 2524-5775 作者: 類似思想 時(shí)間: 2025-3-23 02:23 作者: facilitate 時(shí)間: 2025-3-23 07:52 作者: 抱負(fù) 時(shí)間: 2025-3-23 12:51 作者: 琺瑯 時(shí)間: 2025-3-23 15:08 作者: Grandstand 時(shí)間: 2025-3-23 19:21 作者: 蓋他為秘密 時(shí)間: 2025-3-23 22:45 作者: 溫和女孩 時(shí)間: 2025-3-24 04:41
High Cycle Fatigue and Fatigue Crack Growth Rate in Additive Manufactured Titanium Alloysecimen gauge section. Key findings are as follows. Presence of porosity did not affect the tensile strengths, however both ductility and fatigue strength were significantly reduced. Fatigue life could not be correlated by the applied stress, e.g. in terms of the .-. curves, owing to the different po作者: FEAT 時(shí)間: 2025-3-24 06:47 作者: 保守黨 時(shí)間: 2025-3-24 12:51 作者: ALIAS 時(shí)間: 2025-3-24 15:52
Assessment of Fatigue Behavior of Advanced Aluminum Alloys Under Complex Variable-Amplitude Loadingive load simulating landing in the spectrum crack growth M(T) testing. The special test method employed, results of the equivalency testing, and a comparison to the full-scale panel test results are covered.作者: mitten 時(shí)間: 2025-3-24 19:30 作者: Pseudoephedrine 時(shí)間: 2025-3-25 01:09
An Ultrafast Crack Growth Lifing Model to Support Digital Twin, Virtual Testing, and Probabilistic Doving aircraft design, safety, and reliability..Under Federal Aviation Administration (FAA) Funding, This methodology focused on the development of an ultrafast numerical crack growth algorithm that consists of: (a) a constant amplitude equivalent stress derived from a variable amplitude loading spe作者: nutrition 時(shí)間: 2025-3-25 04:36
Analytical and Numerical Investigation of the Effect of Secondary Bending in Hard-Point Jointsically for typical fuselage configurations was derived as σ./σ.?=?0.20, which is significantly lower than that obtained for lap joint attachments (that can reach up to σ./σ.?=?3.0). An example of an antenna installation is presented, showing significant decrease in the fatigue and crack growth lives作者: 踉蹌 時(shí)間: 2025-3-25 09:55
Demonstration of an Airframe Digital Twin Framework Using a CF-188 Full-Scale Component Testcrack growth predictions. Test cases analysed to verify and validate these modules showed the benefits of the Bayesian updating approach for performing QRA with inputs that are initially scarce and become less uncertain throughout the service life of the aircraft. Short-term benefits expected from t作者: 碌碌之人 時(shí)間: 2025-3-25 12:08 作者: 辮子帶來(lái)幫助 時(shí)間: 2025-3-25 16:15 作者: 過(guò)份艷麗 時(shí)間: 2025-3-25 22:28
implementation. The basic governance provides for a control body that has the task of monitoring the proper functioning of the foundation. The importance of good governance in bank foundations is emphasized by the guidelines drawn up by the ., a voluntary but binding code of conduct common to all fo作者: 腐敗 時(shí)間: 2025-3-26 01:52
Ivan Meneghin,Goran Ivetic,Matthias Stiller,Gianluca Molinari,Vjola Ristori,Sara Della Ratta,Fran?oi as beacons of opportunity and hope; places of empowerment and, in the best, of cultural restitution...In this work, young people interviewed over a span of seven years reflect, in real time, on the intended and unintended consequences boarding has had in their own lives. They relate expected and dr作者: Efflorescent 時(shí)間: 2025-3-26 08:18
Rob Plaskitt,Andrew Halfpenny,Michelle Hill as beacons of opportunity and hope; places of empowerment and, in the best, of cultural restitution...In this work, young people interviewed over a span of seven years reflect, in real time, on the intended and unintended consequences boarding has had in their own lives. They relate expected and dr作者: critique 時(shí)間: 2025-3-26 10:12 作者: 膠水 時(shí)間: 2025-3-26 14:57 作者: Perennial長(zhǎng)期的 時(shí)間: 2025-3-26 18:51 作者: otic-capsule 時(shí)間: 2025-3-26 21:26 作者: curettage 時(shí)間: 2025-3-27 04:11
Guillaume Renaud,Min Liao,Yan Bombardiertice. What emerges is a powerful exposé of political tensions, contestations, and ruptures, inherent to the struggle against the persistent colonizing forces in the lives of oppressed populations. Central to this decolonizing treatise are the paradigmatic transformations essential to an education tr作者: amputation 時(shí)間: 2025-3-27 06:18 作者: 責(zé)怪 時(shí)間: 2025-3-27 11:09
etter understanding of the manner in which foundations interpret strategic planning and reveals?strengths and weaknesses that demand careful attention.978-3-662-51180-0978-3-642-41306-3Series ISSN 1431-1941 Series E-ISSN 2197-716X 作者: 權(quán)宜之計(jì) 時(shí)間: 2025-3-27 17:03 作者: 小卷發(fā) 時(shí)間: 2025-3-27 18:26
Bingfei Liu,Shangyang Jin,Shaozhe Dong,Zhenyu Fengely, .Boasians at War. offers a detailed glimpse of the long troubled history of the concept of race, along with the real-life realities of racism, that have carried on despite the harnessing of scientific knowledge to combat both.?978-3-030-40884-8978-3-030-40882-4作者: cornucopia 時(shí)間: 2025-3-28 01:14 作者: MOCK 時(shí)間: 2025-3-28 02:25 作者: 旅行路線 時(shí)間: 2025-3-28 06:33
2195-4356 nufacturing”, the chapters cover different aspects concerning research, developments and challenges in this field, offering a timely reference guide to designers, regulators, manufacturer, and both researchers and professionals of the broad aerospace community..978-3-030-21505-7978-3-030-21503-3Series ISSN 2195-4356 Series E-ISSN 2195-4364 作者: ETCH 時(shí)間: 2025-3-28 12:36
The Optimization and Design of Complicated-Surface Panel Based on Automate Fiber Placement to simulate the interface between skin and stiffener. With the increase of the number and height of stiffeners, the buckling and post-buckling capacity of double-curvature stiffened panel increases. But the buckling and post-buckling capacity of longitudinal and transverse stiffeners are very close.作者: 勤勉 時(shí)間: 2025-3-28 17:14
Damage Mechanisms and Mechanical Properties of Directly Bonded CFRTP and Aluminium with Nano-Structuicantly compared to two other considered bonding cases. Furthermore, the measured traction-separation behaviour is seen to be difference for each case. Nevertheless, the applied calculation method shows some challenges related to thermal stresses and plastic deformation that should to be taken into account in future studies.作者: facilitate 時(shí)間: 2025-3-28 21:36
Ply Curving Termination to Suppress Delamination in Composite Ply Drop-Offs significantly low stiffness and thus the stress concentration at the ply edge is suppressed. This paper reports the numerical analysis and experiment to validate the effectiveness of this new concept. In addition, suppression of edge delamination by PCT is also demonstrated.作者: 發(fā)出眩目光芒 時(shí)間: 2025-3-29 01:59 作者: 膽小鬼 時(shí)間: 2025-3-29 04:55
2195-4356 ents innovative fatigue life enhancement methods and repair .This book gathers papers presented at the 36.th. conference and 30.th. Symposium of the International Committee on Aeronautical Fatigue and Structural integrity. Focusing on the main theme of “Structural Integrity in the Age of Additive Ma作者: 慷慨不好 時(shí)間: 2025-3-29 10:59 作者: 表示向前 時(shí)間: 2025-3-29 12:39
Fatigue in Additive Manufactured Aircraft: The Long Way to Make It FlyAdditive Manufacturing (AM) or, more colloquially, 3D-printing..As opposed to the conventional subtractive manufacturing methodologies, AM is able to create net-shaped products by means of the addition, layer by layer, of the needed material..The biggest benefit of the AM in respect to the conventio作者: 自制 時(shí)間: 2025-3-29 16:18 作者: NOTCH 時(shí)間: 2025-3-29 19:43 作者: 不可救藥 時(shí)間: 2025-3-30 01:25
The Optimization and Design of Complicated-Surface Panel Based on Automate Fiber Placementure criteria are screened and perfected. Iso-parametric shell element is used to simulate skin and stiffener. A specific interface element is used to simulate between skin and stiffener. During the analysis process of the buckling, post-buckling and failure of the structure under complex loads, the 作者: Facet-Joints 時(shí)間: 2025-3-30 04:05 作者: 迎合 時(shí)間: 2025-3-30 10:31 作者: subacute 時(shí)間: 2025-3-30 14:44
Damage Mechanisms and Mechanical Properties of Directly Bonded CFRTP and Aluminium with Nano-Structunforced thermoplastic (CFRTP) and aluminium. A nanostructure is manufactured on the aluminium surface and is directly bonded to the CFRTP by applying heat and pressure. Double cantilever beam (DCB) testing is carried out to evaluate the bonding properties and the initial results of a method for dire作者: kidney 時(shí)間: 2025-3-30 19:26 作者: 有罪 時(shí)間: 2025-3-30 20:41 作者: insolence 時(shí)間: 2025-3-31 02:45 作者: 分散 時(shí)間: 2025-3-31 06:07 作者: 手榴彈 時(shí)間: 2025-3-31 10:22
Analytical and Numerical Investigation of the Effect of Secondary Bending in Hard-Point Jointss of mechanical fasteners. Upon cabin pressurization, membrane stresses are induced in the skin sheets every flight. Fastened attachments include inherent eccentricity with respect to the load path, which induces out of plane deflections of the skin sheets. This is referred to as ‘secondary bending’作者: 細(xì)查 時(shí)間: 2025-3-31 15:58
Demonstration of an Airframe Digital Twin Framework Using a CF-188 Full-Scale Component Testlow proactive and cost-effective decisions on an individual aircraft basis. The National Research Council of Canada is currently demonstrating the ADT framework using a CF–188 full-scale component test to assess the adaptability of this approach for Royal Canadian Air Force (RCAF) fleets. An in-hous
