Simulation of single-lap bonded and hybrid (bolted/bonded) joints with flexible adhesive
暂无分享,去创建一个
[1] B. Duncan,et al. Hyperelastic modelling of flexible adhesives. , 1999 .
[2] P. K. Mallick,et al. Fatigue of hybrid (adhesive/bolted) joints in SRIM composites , 2001 .
[3] G. Kelly,et al. Quasi-static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints , 2006 .
[4] John Morton,et al. Improved theoretical solutions for adhesive lap joints , 1998 .
[5] Marc Sartor,et al. Hybrid (bolted/bonded) joints applied to aeronautic parts : analytical one-dimensional models of a single-lap joint , 2006 .
[6] Marc Sartor,et al. ANALYTICAL TWO-DIMENSIONAL MODEL OF A HYBRID (BOLTED/BONDED) SINGLE-LAP JOINT , 2007 .
[7] Kosuke Haraga,et al. Fatigue Strength of Adhesive/Rivet Combined Lap Joints , 1995 .
[8] D. J. Allman,et al. A THEORY FOR ELASTIC STRESSES IN ADHESIVE BONDED LAP JOINTS , 1977 .
[9] Du Chen,et al. An Analysis of Adhesive-Bonded Single-Lap Joints , 1983 .
[10] M. C. Niu,et al. Airframe Stress Analysis and Sizing , 2011 .
[11] L. Hart-Smith. Design Methodology for Bonded-Bolted Composite Joints. Volume I. Analysis Derivations and Illustrative Solutions , 1982 .