標(biāo)題: Titlebook: Engineering Against Fracture; Proceedings of the 1 Spiros Pantelakis,Chris Rodopoulos Conference proceedings 2009 Springer Science+Business [打印本頁(yè)] 作者: Taft 時(shí)間: 2025-3-21 20:00
書(shū)目名稱(chēng)Engineering Against Fracture影響因子(影響力)
書(shū)目名稱(chēng)Engineering Against Fracture影響因子(影響力)學(xué)科排名
書(shū)目名稱(chēng)Engineering Against Fracture網(wǎng)絡(luò)公開(kāi)度
書(shū)目名稱(chēng)Engineering Against Fracture網(wǎng)絡(luò)公開(kāi)度學(xué)科排名
書(shū)目名稱(chēng)Engineering Against Fracture被引頻次
書(shū)目名稱(chēng)Engineering Against Fracture被引頻次學(xué)科排名
書(shū)目名稱(chēng)Engineering Against Fracture年度引用
書(shū)目名稱(chēng)Engineering Against Fracture年度引用學(xué)科排名
書(shū)目名稱(chēng)Engineering Against Fracture讀者反饋
書(shū)目名稱(chēng)Engineering Against Fracture讀者反饋學(xué)科排名
作者: averse 時(shí)間: 2025-3-21 21:54 作者: Geyser 時(shí)間: 2025-3-22 01:26 作者: ostensible 時(shí)間: 2025-3-22 06:30
Dynamic Properties and Fatigue Failure of Aircraft Component parameters at presence of elastic supporting of the beam and the attached additional concentrated weight. A result of dynamic analysis has a good correlation with the fatigue damages observed at fatigue test of a beam.作者: cumber 時(shí)間: 2025-3-22 10:19 作者: Intentional 時(shí)間: 2025-3-22 16:14 作者: Intentional 時(shí)間: 2025-3-22 21:08
Next Generation Composite Aircraft Fuselage Materials under Post-crash Fire Conditionseratures at various points through the thickness..Modelling the thermal and structural behaviour under load required the use of a modified version of the Henderson Equation, which describes heat transfer through composites under ablative fire conditions. This has been incorporated into the Com-Fire 作者: 陶瓷 時(shí)間: 2025-3-22 23:35 作者: Resistance 時(shí)間: 2025-3-23 05:14 作者: Incommensurate 時(shí)間: 2025-3-23 07:17 作者: 拉開(kāi)這車(chē)床 時(shí)間: 2025-3-24 06:06 作者: NIB 時(shí)間: 2025-3-24 06:49 作者: Bronchial-Tubes 時(shí)間: 2025-3-24 12:39 作者: OASIS 時(shí)間: 2025-3-24 17:08
Conference proceedings 2009e was not easy and de?nitely, not something that was brought to life without a lot of work and c- st mitment. The 1 Conference of Engineering Against Fracture from its conceptual day until completion was designed in a way of underlying the need of bringing all the key players on a common ground that作者: Diverticulitis 時(shí)間: 2025-3-24 21:52 作者: V洗浴 時(shí)間: 2025-3-25 00:58
,Die Talsperrenme?technik in der Praxis,tures. Damage detection is by far being automatic since not all defects are dangerous. The correct diagnostics require not only a knowledge of the size of the prevailing defects but also their likely locations of occurrence from the initial design and/or past experience. What is not known is the tim作者: Invigorate 時(shí)間: 2025-3-25 05:35
https://doi.org/10.1007/978-3-662-13080-3ve steels which would possess high-strength combined with high formability while these steels could also exhibit high fracture and fatigue resistance. Especially for the automotive industry, the driving force for these developments is the vehicle weight reduction, which could eventually lead to lowe作者: 性冷淡 時(shí)間: 2025-3-25 07:50
Von New-York nach Philadelphia, fuselage structures. Following a screening of the static, fatigue and damage tolerance performances of thin MLs coupons an investigation, focused on identification of fuselage areas best suited for ML application has been performed. After a weight optimization analysis large panel tests have been d作者: capillaries 時(shí)間: 2025-3-25 14:40
Matthias Book,Volker Gruhn,Rüdiger Striemerfuel consumption. The use of such advanced materials and technologies tends to increase the cost. Multifunctional materials (MFMs) and related processing technologies aim at overcoming this increase of cost by exploiting the high level of functional integration. MFMs are designed so as to meet speci作者: 極大的痛苦 時(shí)間: 2025-3-25 16:26
ne) (SABIC PP 108MF10, SABIC PP 33 MBTU [Saudi Basic Industries Corporation]) composite matrix. A range of mechanical properties were measured (tensile test, bending test, fracture toughness, notched impact strength (at the ambient temperature and ?20°C), strain at break, impact strength), as well a作者: 對(duì)待 時(shí)間: 2025-3-25 22:13 作者: Corroborate 時(shí)間: 2025-3-26 00:08 作者: 任命 時(shí)間: 2025-3-26 07:21
Threads in an Object-Oriented World,hanical systems dynamics at non-classic internal and external constraints. The method of the concentrated weights is convenient means of the analysis of dynamic properties of elastic mechanical systems. It has relative simplicity of definition of the parameters of equivalent discrete system, the cle作者: 材料等 時(shí)間: 2025-3-26 09:25
Preliminary Information Gathering-corroded specimens. The S-N curve of the parent material exhibits a very smooth transition from low to high cycle fatigue regime indicating a strong stress sensitivity. Crack initiation occurs already at early stage of the fatigue damage accumulation process. A transgranular initiation fracture is 作者: 統(tǒng)治人類(lèi) 時(shí)間: 2025-3-26 16:14 作者: 愚蠢人 時(shí)間: 2025-3-26 17:03
Profit Sharing and Co-Partnershipr under a heat flux of 75kW m.. It was found, for the first time, that stress has a small but significant effect on the fire reaction properties. Increasing tensile stress increased heat release rate and smoke production, while shortening the time-to-ignition. Compressive stress had the reverse effe作者: 沐浴 時(shí)間: 2025-3-26 22:46 作者: ARBOR 時(shí)間: 2025-3-27 04:33
Stephen R. D. Johnston,Mitchell Dowsettuctures..The US Federal Aviation Administration regulations for the penetration of an external fuel fire into an aircraft cabin after crash require a burn-through period of 4min (FAA § 25.856 Appendix F, Part VII). Different candidate structures for the next generation of composite aircraft fuselage作者: MARS 時(shí)間: 2025-3-27 06:23 作者: auxiliary 時(shí)間: 2025-3-27 12:11
A.H.B. Schuurs,J.P. van Amerongenradation and fatigue life under multi-axial loading. Non-crimp-fabrics (NCF) consist of several sub-layers with different orientations, all stitched together by a stitching yarn. Its lay-up can be tailored to specific needs. It offers cost-savings in production processes because instead of laying se作者: exhilaration 時(shí)間: 2025-3-27 15:22
Vervangen van een defecte onlayrestauratie, model has been implemented and upgraded to account for the local material properties of the pre-corroded material ahead of the crack tip. In the model the local fracture behaviour at the crack tip of the corroded alloy is governed by the local fracture toughness of the material. The analytical resu作者: prolate 時(shí)間: 2025-3-27 18:25 作者: Osteons 時(shí)間: 2025-3-28 00:11
https://doi.org/10.1007/978-3-319-89303-7ndaries, crystallographic orientations, phases, etc. Crystallographic orientations of grains is one such feature and it’s influence on the crack tip opening displacements (CTOD) of a small crack is investigated in presented work. The principal objective is to ascertain the difference in influence of作者: Orthodontics 時(shí)間: 2025-3-28 02:24
978-90-481-8119-3Springer Science+Business Media B.V. 2009作者: SLING 時(shí)間: 2025-3-28 09:51
Der Talsperrenbau in Deutschland,ning during burnishing respond very beneficially with regard to HCF performance while others which show little work-hardening may even react with losses in HCF strength. Possible explanations for such behavior are outlined in terms of mean stress and environmental sensitivities of the fatigue strengths of the various materials and microstructures.作者: Albinism 時(shí)間: 2025-3-28 13:09
Ball-Burnishing and Roller-Burnishing to Improve Fatigue Performance of Structural Alloysning during burnishing respond very beneficially with regard to HCF performance while others which show little work-hardening may even react with losses in HCF strength. Possible explanations for such behavior are outlined in terms of mean stress and environmental sensitivities of the fatigue strengths of the various materials and microstructures.作者: Epithelium 時(shí)間: 2025-3-28 16:09
Spiros Pantelakis,Chris RodopoulosIntegrated solution approach.Future technologies.Existing problems.Pin-pointing problems and gaps in need of a solution.Examples for practice作者: Resection 時(shí)間: 2025-3-28 20:55
http://image.papertrans.cn/e/image/310692.jpg作者: maudtin 時(shí)間: 2025-3-29 00:11
https://doi.org/10.1007/978-1-4020-9402-6Retarder; alloy; crystal; damage; fatigue; fracture; fracture mechanics; magnesium; mechanics; modeling; polym作者: Flavouring 時(shí)間: 2025-3-29 05:26 作者: 最初 時(shí)間: 2025-3-29 11:02
Dual Scale Fatigue Crack Monitoring Scheme Considering Random Material, Geometric and Load Charactertures. Damage detection is by far being automatic since not all defects are dangerous. The correct diagnostics require not only a knowledge of the size of the prevailing defects but also their likely locations of occurrence from the initial design and/or past experience. What is not known is the tim作者: CORD 時(shí)間: 2025-3-29 11:39 作者: inscribe 時(shí)間: 2025-3-29 18:10
Hybrid Metal Laminates for Low Weight Fuselage Structures fuselage structures. Following a screening of the static, fatigue and damage tolerance performances of thin MLs coupons an investigation, focused on identification of fuselage areas best suited for ML application has been performed. After a weight optimization analysis large panel tests have been d作者: 寬容 時(shí)間: 2025-3-29 20:24 作者: DEAWL 時(shí)間: 2025-3-30 00:55
Effect of Talc Filler Content on Poly(Propylene) Composite Mechanical Propertiesne) (SABIC PP 108MF10, SABIC PP 33 MBTU [Saudi Basic Industries Corporation]) composite matrix. A range of mechanical properties were measured (tensile test, bending test, fracture toughness, notched impact strength (at the ambient temperature and ?20°C), strain at break, impact strength), as well a作者: 壁畫(huà) 時(shí)間: 2025-3-30 06:22 作者: deriver 時(shí)間: 2025-3-30 08:13
Influence of Width of Specimen on Tensile Properties of NiCo Thin Filmtester developed by authors was used to measure the mechanical characteristics of thin film materials. The tester has a load cell with maximum capacity of 0.5N and a non-contact position measuring system based on the principle of capacitance micrometry. The “dog-bone” type specimen was designed and 作者: yohimbine 時(shí)間: 2025-3-30 12:22
Dynamic Properties and Fatigue Failure of Aircraft Componenthanical systems dynamics at non-classic internal and external constraints. The method of the concentrated weights is convenient means of the analysis of dynamic properties of elastic mechanical systems. It has relative simplicity of definition of the parameters of equivalent discrete system, the cle作者: Adherent 時(shí)間: 2025-3-30 18:43
Investigation of the Fatigue Behaviour of the Structural Magnesium Alloy AZ31-corroded specimens. The S-N curve of the parent material exhibits a very smooth transition from low to high cycle fatigue regime indicating a strong stress sensitivity. Crack initiation occurs already at early stage of the fatigue damage accumulation process. A transgranular initiation fracture is 作者: 藝術(shù) 時(shí)間: 2025-3-30 21:27
Coulomb Failure Surfaces in Ductile Non Linear Elastic Materialsiple of Conservation of Energy — the total elastic strain energy density in this case. This Principle is equivalent to the path-independence of strain energy, the same not being true for its components, i.e. dilatational and distortional densities. This way, an intimate quantitative relationship is 作者: Flounder 時(shí)間: 2025-3-31 01:52
Effect of Stress on the Fire Reaction Properties of Polymer Composite Laminatesr under a heat flux of 75kW m.. It was found, for the first time, that stress has a small but significant effect on the fire reaction properties. Increasing tensile stress increased heat release rate and smoke production, while shortening the time-to-ignition. Compressive stress had the reverse effe作者: RAFF 時(shí)間: 2025-3-31 05:24 作者: 騷擾 時(shí)間: 2025-3-31 09:37 作者: 杠桿 時(shí)間: 2025-3-31 14:48 作者: 憲法沒(méi)有 時(shí)間: 2025-3-31 17:36 作者: PACK 時(shí)間: 2025-3-31 22:02
Fatigue Crack Growth Assessment of Corroded Aluminum Alloys model has been implemented and upgraded to account for the local material properties of the pre-corroded material ahead of the crack tip. In the model the local fracture behaviour at the crack tip of the corroded alloy is governed by the local fracture toughness of the material. The analytical resu作者: integral 時(shí)間: 2025-4-1 02:02
Fatigue Crack Growth Behavior under Spectrum Loadingtary P-3 cargo airplane. The material is 2324 — T39 Al alloy widely used in the aircraft industry. Experiments were conducted using the full spectrum and modified versions of it such as only ‘positive’ (no negative loads) or with reduced (clipped) high peaks. The results show that the compressive lo作者: Gudgeon 時(shí)間: 2025-4-1 08:52 作者: 數(shù)量 時(shí)間: 2025-4-1 12:27 作者: 兒童 時(shí)間: 2025-4-1 17:57 作者: Tortuous 時(shí)間: 2025-4-1 22:33
Progressive Fracture Analysis of Planar Lattices and Shape-Morphing Kagome Structureh of the lattices. On the other hand, with increasing the load in the Kagome structure, yielding and buckling of the struts in the core and yielding of the face-sheet appear consecutively inducing degradation of structure’s bending stiffness and large dips of the loaded end.作者: CRACK 時(shí)間: 2025-4-2 02:17
Fatigue Behavior of Non-crimp Fabricsveral single layers under different orientations into a mould it is possible to lay just one NCF that includes all sublayers. One disadvantage is the stitching that causes local inhomogenities and fiber misalignment in the material.作者: 撫育 時(shí)間: 2025-4-2 03:48
Fatigue Crack Growth Assessment of Corroded Aluminum Alloyslts obtained show good correlation with fatigue crack growth experiments under irregular aircraft service spectra from the literature and demonstrate the significance to consider the degradation of local material properties of structural members including corroded areas.作者: 有角 時(shí)間: 2025-4-2 10:42 作者: 糾纏,纏繞 時(shí)間: 2025-4-2 11:30 作者: 鞠躬 時(shí)間: 2025-4-2 17:07
