000109234 001__ 109234
000109234 005__ 20190117190708.0
000109234 0247_ $$2doi$$a10.1016/j.compositesb.2004.11.002
000109234 022__ $$a1359-8368
000109234 02470 $$2DAR$$a6644
000109234 02470 $$a000227825900006$$2ISI
000109234 037__ $$aARTICLE
000109234 245__ $$aAdhesively bonded lap joints from pultruded GFRP profiles. Part II: joint strength prediction
000109234 260__ $$c2005
000109234 269__ $$a2005
000109234 336__ $$aJournal Articles
000109234 520__ $$aA method to predict the strength of adhesively bonded single and double lap joints from pultruded GFRP composite adherends subjected to quasi-static axial tensile loading is presented. The method is based on a quadratic through- thickness shear-tensile interaction failure criterion. The failure criterion was deduced from measured combined through-thickness tensile and shear strength values in the outer fiber-mat layer of the adherends (locations of the ultimate failure). The experimental strength values were obtained from a new shear-tensile interaction device (STI- device), which allows the measurement of shear-tensile interaction strength values. The predicted joint strengths corresponded well to the measured joint strengths of adhesively bonded single and double lap joints with different geometrical configurations. The investigation also showed that the material strength depended on the expansion of the stressed surface. The resistance against local stress peaks was much higher than the resistance against large uniformly distributed stress blocks. The application of the ultimate failure load prediction method showed a small influence of the adhesive layer thickness on the joint strength although the influence of the fillet radius was seen to be much higher. A partial material safety factor for the joint strength of 1.34 was determined. [All rights reserved Elsevier]
000109234 6531_ $$aAdhesive bonding
000109234 6531_ $$aFilled polymers
000109234 6531_ $$aGlass fibre reinforced plastics
000109234 6531_ $$aMechanical testin
000109234 6531_ $$aShear strength
000109234 6531_ $$aStress analysis
000109234 6531_ $$aTensile strength
000109234 700__ $$0240002$$g121845$$aKeller, T.
000109234 700__ $$0240889$$g140184$$aVallée, T.
000109234 773__ $$j36$$tComposites Part B$$k4$$q341-350
000109234 909C0 $$xU10234$$0252002$$pCCLAB
000109234 909CO $$particle$$pENAC$$ooai:infoscience.tind.io:109234
000109234 917Z8 $$x229997
000109234 917Z8 $$x229997
000109234 917Z8 $$x229997
000109234 937__ $$aCCLAB-ARTICLE-2005-006
000109234 970__ $$a53/CCLAB
000109234 973__ $$rREVIEWED$$sPUBLISHED$$aEPFL
000109234 980__ $$aARTICLE