標(biāo)題: Titlebook: Dynamic Failure of Composite and Sandwich Structures; Serge Abrate,Bruno Castanié,Yapa D. S. Rajapakse Book 2013 Springer Science+Business [打印本頁] 作者: Agoraphobia 時(shí)間: 2025-3-21 16:41
書目名稱Dynamic Failure of Composite and Sandwich Structures影響因子(影響力)
書目名稱Dynamic Failure of Composite and Sandwich Structures影響因子(影響力)學(xué)科排名
書目名稱Dynamic Failure of Composite and Sandwich Structures網(wǎng)絡(luò)公開度
書目名稱Dynamic Failure of Composite and Sandwich Structures網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Dynamic Failure of Composite and Sandwich Structures被引頻次
書目名稱Dynamic Failure of Composite and Sandwich Structures被引頻次學(xué)科排名
書目名稱Dynamic Failure of Composite and Sandwich Structures年度引用
書目名稱Dynamic Failure of Composite and Sandwich Structures年度引用學(xué)科排名
書目名稱Dynamic Failure of Composite and Sandwich Structures讀者反饋
書目名稱Dynamic Failure of Composite and Sandwich Structures讀者反饋學(xué)科排名
作者: miracle 時(shí)間: 2025-3-22 00:10
,Berechnung statisch unbestimmter Tr?ger, of composite sandwich structures with CFRP skins compared to GFRP equivalent constructions is demonstrated for air-blast experiments. Strain gauges were used to monitor the structural response of similar sandwich materials and GFRP tubular laminates during underwater shocks. The effect of the suppo作者: Gerontology 時(shí)間: 2025-3-22 01:13
,Unterstützende Beatmungsverfahren,pressive strength, failed from impact at 300 m/s; but the carbon laminates developed shear cracks above 10% of the ultimate compressive strength. The work is of benefit to naval and other composite designers to be able to account for failure envelopes under complex dynamic loading states, i.e. pre-s作者: 反省 時(shí)間: 2025-3-22 05:04 作者: intrigue 時(shí)間: 2025-3-22 12:31
Sedonalgesierung bei Langzeitbeatmeten,eloped to verify the hypothesis of the analytical model. The model showed good agreement with experimental results for a laminate thickness between 3 and 6 mm. However, when the thickness reached 12 mm the model overestimated the residual velocity of the projectile..The validated analytical model is作者: 壯觀的游行 時(shí)間: 2025-3-22 14:22
Reinhard Larsen,Thomas Ziegenfu?el. The fiber failure model was set up using an original formulation between the integration points of the volume element in order to dissipate a constant energy release rate per unit area. Finally the model was used to evaluate the distribution of the dissipated energy among the different damage ty作者: 壯觀的游行 時(shí)間: 2025-3-22 20:05
Reinhard Larsen,Thomas Ziegenfu?ental response has also been compared with predictions from the FE model and the analytical models using various material models of the ice. FE models using a calibrated elastic–plastic ice model are capable of accurately predicting the response and delamination initiation, while the current analyti作者: intention 時(shí)間: 2025-3-23 01:01 作者: Femish 時(shí)間: 2025-3-23 05:14
ere performed. These experimental results are reported together with numerical simulation ones. The main idea of the research was to demonstrate energy absorbing capabilities of a thin-walled crash box during the frontal impact, with the lowest initial deceleration. In order to initialize the collap作者: Opponent 時(shí)間: 2025-3-23 05:51
wever experimentation is sometimes complicated by the size of structures. The similitude techniques can then provide a solution. Similitude techniques are used to study composite materials subjected to impact. We propose here an approach allowing modeling and numerical simulation validated on an ind作者: 充滿裝飾 時(shí)間: 2025-3-23 13:22 作者: LITHE 時(shí)間: 2025-3-23 17:23 作者: 令人苦惱 時(shí)間: 2025-3-23 18:30
Hydroelastic Impacts of Deformable Wedges,odies, the dynamic deflection could interact with the fluid flow, affecting the hydrodynamic load. This work investigates the hull-slamming problem by experiments and numerical simulations of the water entry of elastic wedges impacting on an initially calm surface with pure vertical velocity. The ob作者: anthesis 時(shí)間: 2025-3-23 23:26 作者: CAJ 時(shí)間: 2025-3-24 02:39 作者: 閑蕩 時(shí)間: 2025-3-24 07:22
Damage Mechanisms and Energy Absorption in Composite Laminates Under Low Velocity Impact Loads,ems varying the initial kinetic energy until the complete penetration. This allows the study of the start and propagation of the failure modes. From the load-deflection curves recorded, all the impact parameters involved like first failure and maximum load and energy, absorbed and penetration energy作者: OCTO 時(shí)間: 2025-3-24 13:14 作者: 勤勞 時(shí)間: 2025-3-24 16:47
Discrete Impact Modeling of Inter- and Intra-laminar Failure in Composites,el. The fiber failure model was set up using an original formulation between the integration points of the volume element in order to dissipate a constant energy release rate per unit area. Finally the model was used to evaluate the distribution of the dissipated energy among the different damage ty作者: PTCA635 時(shí)間: 2025-3-24 20:48 作者: Protein 時(shí)間: 2025-3-24 23:20 作者: Lignans 時(shí)間: 2025-3-25 05:48 作者: 大喘氣 時(shí)間: 2025-3-25 11:18
Composites and Dynamic Failures: Experimental and Numerical Solving Strategies and Solutions,wever experimentation is sometimes complicated by the size of structures. The similitude techniques can then provide a solution. Similitude techniques are used to study composite materials subjected to impact. We propose here an approach allowing modeling and numerical simulation validated on an ind作者: Genome 時(shí)間: 2025-3-25 14:50 作者: fibroblast 時(shí)間: 2025-3-25 18:16 作者: 樹膠 時(shí)間: 2025-3-25 21:18
0925-0042 ive assessments of the literature and new developments.Conta.This book presents a broad view of the current state of the art regarding the dynamic response of composite and sandwich structures subjected to impacts and explosions. Each chapter combines a thorough assessment of the literature with ori作者: legislate 時(shí)間: 2025-3-26 01:21 作者: Medicare 時(shí)間: 2025-3-26 07:26 作者: 廢墟 時(shí)間: 2025-3-26 12:03
Reinhard Larsen,Thomas Ziegenfu?or on sandwiches very well. This approach provides an understanding of how the sandwich and the core behave under compression after impact. An original criterion based on a local core crush is tested and validated to compute the residual strength. To consider the bending response of sandwich structures, a multi-level approach is also proposed.作者: 為寵愛 時(shí)間: 2025-3-26 14:07
https://doi.org/10.1007/978-94-017-6297-7ems related to the size of the modeled structure, original modeling strategies are developed to accurately represent the damage observed. The calculated impact behavior and amount of damage are validated by comparison with experimental test results.作者: Expand 時(shí)間: 2025-3-26 18:34
Interaction of Underwater Blasts and Submerged Structures,It provides great insight into the physics of the problem and explains the evolution of the shape of the various fronts and the formation of singularities. Applications to the medical field are also presented.作者: Evolve 時(shí)間: 2025-3-26 22:55
Discrete Modeling of the Crushing of Nomex Honeycomb Core and Application to Impact and Post-impactor on sandwiches very well. This approach provides an understanding of how the sandwich and the core behave under compression after impact. An original criterion based on a local core crush is tested and validated to compute the residual strength. To consider the bending response of sandwich structures, a multi-level approach is also proposed.作者: Stress 時(shí)間: 2025-3-27 02:12 作者: 疲勞 時(shí)間: 2025-3-27 07:38 作者: Immunotherapy 時(shí)間: 2025-3-27 11:34
Serge Abrate,Bruno Castanié,Yapa D. S. RajapakseDiscusses a wide range of topics dealing with explosions and impact in marine, aerospace and transportation applications.Presents comprehensive assessments of the literature and new developments.Conta作者: Excitotoxin 時(shí)間: 2025-3-27 14:41 作者: Cytology 時(shí)間: 2025-3-27 19:58
https://doi.org/10.1007/978-94-007-5329-7Composite materials; Explosions; Hull slamming; Impact on composite structures; Marine structures; Sandwi作者: Coeval 時(shí)間: 2025-3-28 00:32
978-94-017-7951-7Springer Science+Business Media Dordrecht 2013作者: placebo 時(shí)間: 2025-3-28 03:03
Dynamic Failure of Composite and Sandwich Structures978-94-007-5329-7Series ISSN 0925-0042 Series E-ISSN 2214-7764 作者: Conflict 時(shí)間: 2025-3-28 09:56
,Kippen und Verdrillen von Tr?gern, their similarity to a generic hull section. Hull slamming occurs when a ship re-enters the water after having been partially or completely lifted out the water. There are three more cases commonly defined as slamming phenomena: bow-flare, wet-deck and green water slamming. These are all special cas作者: 勉勵(lì) 時(shí)間: 2025-3-28 14:28
,Berechnung statisch unbestimmter Tr?ger,te materials and laminate composite tubes. Explosive charges of 0.64–100 kg TNT equivalent were used during these air- and underwater-blast tests. The difference in response and damage inflicted from underwater- and air-blast loading was assessed from strain-field measurements and post-blast specime作者: 夾克怕包裹 時(shí)間: 2025-3-28 15:58
CERN and the Taming of the Zoo,water, or a liquid with a different speed of sound are considered and the specific issue considered is the prediction of the position of the various wave fronts as a function of time. This is a challenging problem for both analytical and numerical approaches due to the sharp discontinuities, the com作者: 入伍儀式 時(shí)間: 2025-3-28 18:55 作者: 打火石 時(shí)間: 2025-3-29 02:59 作者: Precursor 時(shí)間: 2025-3-29 06:58
https://doi.org/10.1007/978-3-540-88812-3 the complex mechanisms of damage initiation and propagation under low velocity impact loads. A review of the main results is hereafter presented..The problem is that many parameters are involved in an impact and the induced damage is very complex and not always visible. The present research efforts作者: FLORA 時(shí)間: 2025-3-29 10:52
Sedonalgesierung bei Langzeitbeatmeten, scientific literature to model the behavior of composite laminates subjected to high-velocity impact of low-mass projectiles is presented, and a new analytical model is proposed. The present model is able to predict the energy absorbed by the laminate during the perforation process including the ma作者: Noctambulant 時(shí)間: 2025-3-29 14:02 作者: 小母馬 時(shí)間: 2025-3-29 19:25 作者: CLASH 時(shí)間: 2025-3-29 23:16
Reinhard Larsen,Thomas Ziegenfu? the demonstration that Nomex honeycomb behaves in a post-buckling mode very early and that compression forces are taken up by the corners or vertical edges of the honeycomb cells in the same way as they are in the stiffeners in aircraft structures. Thus it is possible to represent the honeycomb dis作者: Incompetent 時(shí)間: 2025-3-30 03:10
Reinhard Larsen,Thomas Ziegenfu?es are produced by folding a flat sheet of material to three-dimensional zigzag structures in an origami-like manner. Relevant cell wall materials range from cardboard to plastics, from metals to composites. Different manufacturing processes and feasible cellular configurations are presented based o
