Investigation the effect of tightening torque on the fatigue strength of double lap simple bolted and hybrid (bolted–bonded) joints using volumetric method
暂无分享,去创建一个
[1] W. Chan,et al. Analysis of Composite Bonded/Bolted Joints Used in Repairing , 2001 .
[2] J. Onõro,et al. A simple mechanical model of a structural hybrid adhesive/riveted single lap joint , 2007 .
[3] Zainul Huda,et al. Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft , 2010 .
[4] T. N. Chakherlou,et al. ON THE FATIGUE BEHAVIOR OF COLD EXPANDED FASTENER HOLES SUBJECTED TO BOLT TIGHTENING , 2011 .
[5] S. Hosseini-Hashemi,et al. Flutter stabilization of cantilevered plates using a bonded patch , 2011 .
[6] R. Heywood. Designing Against Fatigue , 1962 .
[7] J. Keith Nisbett,et al. Shigley's Mechanical Engineering Design , 1983 .
[8] Jeffrey Vogwell,et al. The effect of bolt clamping force on the fracture strength and the stress intensity factor of a plate containing a fastener hole with edge cracks , 2009 .
[9] Tanja Neumann,et al. Fracture And Fatigue Emanating From Stress Concentrators , 2016 .
[10] P. K. Mallick,et al. Fatigue of hybrid (adhesive/bolted) joints in SRIM composites , 2001 .
[11] H Adib,et al. Theoretical and numerical aspects of the volumetric approach for fatigue life prediction in notched components , 2003 .
[12] Erdogan Madenci,et al. Analysis of bolted–bonded composite single-lap joints under combined in-plane and transverse loading , 2009 .
[13] M. Zehsaz,et al. Fatigue Life Prediction of Notched Specimens using the Volumetric Approach , 2011 .
[14] Mohammad Zehsaz,et al. Spot weld arrangement effects on the fatigue behavior of multi-spot welded joints , 2011 .
[15] A. Al-Samhan. Analysis of Adhesively Bonded Riveted Joints , 2005 .
[16] J. D. Clarke,et al. Use of adhesives in repair of cracks in ship structures , 1988 .
[17] G. Kelly,et al. LOAD TRANSFER IN HYBRID (BONDED/BOLTED) COMPOSITE SINGLE-LAP JOINTS , 2005 .
[18] G. Kelly,et al. Quasi-static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints , 2006 .
[19] Mir Jalil Razavi,et al. An experimental investigation of the bolt clamping force and friction effect on the fatigue behavior of aluminum alloy 2024-T3 double shear lap joint , 2011 .
[20] H. Neuber. Theory of notch stresses : principles for exact calculation of strength with reference to structural form and material , 1958 .
[21] Fu-Kuo Chang,et al. Experimental study on clamping effects on the tensile strength of composite plates with a bolt-filled hole , 1999 .
[22] T. N. Chakherlou,et al. Reduction in clamping force due to applied longitudinal load to aerospace structural bolted plates , 2009 .
[23] R. Peterson,et al. Stress Concentration Factors , 1974 .
[24] Onur Sayman,et al. Experimental failure analysis of mechanically fastened joints with clearance in composite laminates under preload , 2008 .
[25] T. Chakherlou,et al. Investigating clamping force variations in Al2024-T3 interference fitted bolted joints under static and cyclic loading , 2012 .
[26] A. Bahkali,et al. FINITE ELEMENT MODELING FOR THERMAL STRESSES DEVELOPED IN RIVETED AND RIVET-BONDED JOINTS , 2011 .
[27] Marc Sartor,et al. ANALYTICAL TWO-DIMENSIONAL MODEL OF A HYBRID (BOLTED/BONDED) SINGLE-LAP JOINT , 2007 .
[28] L. Hart-Smith. Bonded-Bolted Composite Joints , 1985 .
[29] Mohammad Zehsaz,et al. Investigating the effect of clamping force on the fatigue life of bolted plates using volumetric approach , 2013 .
[30] A. Pirondi,et al. Clinch-Bonded and Rivet-Bonded Hybrid Joints: Application of Damage Models for Simulation of Forming and Failure , 2009 .