Scott Fawaz
Scott Fawaz
President, SAFE Inc.
Verified email at saf-engineering.com - Homepage
Title
Cited by
Cited by
Year
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
831998
Fatigue crack growth in riveted joints
SA Fawaz
601997
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
572003
Stress intensity factor solutions for part-elliptical through cracks
SA Fawaz
Engineering Fracture Mechanics 63 (2), 209-226, 1999
571999
Accurate stress intensity factor solutions for corner cracks at a hole
SA Fawaz, B Andersson
Engineering Fracture Mechanics 71 (9-10), 1235-1254, 2004
492004
Equivalent initial flaw size testing and analysis
SA Fawaz
AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH AIR VEHICLES DIRECTORATE, 2000
252000
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
212018
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
212016
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
202016
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
182005
A thin-sheet, combined tension and bending specimen
SA Fawaz, JJM De Rijck
Experimental mechanics 39 (3), 171-176, 1999
171999
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, 187-207, 2009
142009
Stress intensity factors and crack interaction in adjacent holes
JJM De Rijck, SA Fawaz
Engineering Fracture Mechanics 68 (7), 963-969, 2001
132001
1 Accurate Stress Intensity Factor Solutions for Unsymmetric Corner Cracks at a Hole
SA Fawaz, B Andersson
132000
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
131997
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
112003
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
112000
Fatigue crack growth in riveted joints. Diss
SA Fawaz
Delft University of Technology, 1997
111997
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, 1035-1068, 2009
82009
The effect of dents in fuselage structures on fatigue and static stability
C Guijt, D Hill, J Rausch, S Fawaz
ICAF Conference, 2005
82005
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