Agoraphobia 发表于 2025-3-21 16:41:10
书目名称Dynamic Failure of Composite and Sandwich Structures影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0283585<br><br> <br><br>书目名称Dynamic Failure of Composite and Sandwich Structures读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0283585<br><br> <br><br>miracle 发表于 2025-3-22 00:10:21
,Berechnung statisch unbestimmter Träger, 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 suppoGerontology 发表于 2025-3-22 01:13:08
,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反省 发表于 2025-3-22 05:04:21
http://reply.papertrans.cn/29/2836/283585/283585_4.pngintrigue 发表于 2025-3-22 12:31:52
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壮观的游行 发表于 2025-3-22 14:22:48
Reinhard Larsen,Thomas Ziegenfußel. 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壮观的游行 发表于 2025-3-22 20:05:08
Reinhard Larsen,Thomas Ziegenfußental 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 analytiintention 发表于 2025-3-23 01:01:34
http://reply.papertrans.cn/29/2836/283585/283585_8.pngFemish 发表于 2025-3-23 05:14:40
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 collapOpponent 发表于 2025-3-23 05:51:35
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