Application of the virtual crack closure technique to calculate stress intensity factors for through cracks with an elliptical crack front SA Fawaz Engineering Fracture Mechanics 59 (3), 327-342, 1998 | 101 | 1998 |
Fatigue crack growth in riveted joints SA Fawaz | 68 | 1997 |
Equivalent initial flaw size testing and analysis of transport aircraft skin splices SA FAWAZ Fatigue & Fracture of Engineering Materials & Structures 26 (3), 279-290, 2003 | 63 | 2003 |
Stress intensity factor solutions for part-elliptical through cracks SA Fawaz Engineering Fracture Mechanics 63 (2), 209-226, 1999 | 61 | 1999 |
Accurate stress intensity factor solutions for corner cracks at a hole SA Fawaz, B Andersson Engineering Fracture Mechanics 71 (9-10), 1235-1254, 2004 | 60 | 2004 |
Effect of electrical discharge machining on corrosion and corrosion fatigue behavior of aluminum alloys SR Arunachalam, SEG Dorman, RT Buckley, NA Conrad, SA Fawaz International Journal of Fatigue 111, 44-53, 2018 | 38 | 2018 |
Test method for corrosion pit-to-fatigue crack transition from a corner of hole in 7075-T651 aluminum alloy S Arunachalam, S Fawaz International Journal of Fatigue 91, 50-58, 2016 | 38 | 2016 |
Stress intensity factors of various size single edge-cracked tension specimens: A review and new solutions MJ Hammond, SA Fawaz Engineering Fracture Mechanics 153, 25-34, 2016 | 35 | 2016 |
Equivalent initial flaw size testing and analysis SA Fawaz Ohio USA: Air Force Research Laboratory.(Report Nr AFRL-VA-TR-2000-3024) 10, 2000 | 30 | 2000 |
Compilation of damage findings from multiple recent teardown analysis programs GA Shoales, SA Fawaz, MR Walters ICAF 2009, Bridging the Gap between Theory and Operational Practice …, 2009 | 26 | 2009 |
A thin-sheet, combined tension and bending specimen SA Fawaz, JJM De Rijck Experimental mechanics 39, 171-176, 1999 | 19 | 1999 |
A risk assessment methodology and tool for probabilistic damage tolerance-based maintenance planning M Shiao, K Boyd, S Fawaz 8th FAA/NASA/DoD Aging Aircraft Conference, 2005 | 18 | 2005 |
Accurate stress intensity factor solutions for unsymmetric corner cracks at a hole SA Fawaz, B Andersson Flygtekniska Försöksanstalten, 2000 | 16 | 2000 |
The effect of dents in fuselage structures on fatigue and static stability C Guijt, D Hill, J Rausch, S Fawaz International committee on aeronautical fatigue (ICAF) conference, Hamburg …, 2005 | 14 | 2005 |
Stress intensity factors and crack interaction in adjacent holes JJM De Rijck, SA Fawaz Engineering Fracture Mechanics 68 (7), 963-969, 2001 | 14 | 2001 |
Experimental verification of stress intensity factor solutions for corner cracks at a hole subject to general loading SA Fawaz, B Andersson, JC Newman Jr Proceedings of the 22nd symposium of the international committee on …, 2003 | 13 | 2003 |
A simplified approach for stress analysis of mechanically fastened joints JJM De Rijck, SA Fawaz 4th Joint DoD/FAA/NASA Conference on Aging Aircraft, 2000 | 13 | 2000 |
Fatigue crack growth in riveted joints. Diss SA Fawaz Delft University of Technology, 1997 | 13 | 1997 |
Fatigue crack growth in riveted lap-splice joints SA Fawaz, J Schijve, AU de Koning Proc. of the 19th Symposium of the International Committee on Aeronautical …, 1997 | 12 | 1997 |
Three Diminsional Crack Growth Prediction SE Galyon, SR Arunachalam, J Greer, M Hammond, SA Fawaz ICAF 2009, Bridging the Gap between Theory and Operational Practice …, 2009 | 8 | 2009 |