Galyon Dorman, S. E., Justin W. Rausch, Jason H. J. H. Niebuhr, S. R. Arunachalam, S. A. Fawaz, Adam Goff (Luna Innovations), and Jesse C. Kelly (Luna Innovations). (2018). Effect of Galvanic Coupling and Corrosion Inhibiting Coatings on Environmentally Assisted Cracking. SAFE, Inc.
Robert G. Kelly, Saravanan Arunachalam, Stephanie L. Kaster, Richard T. Buckley and Scott A. Fawaz (2017). Mechanical Impact of Corrosion Damage. 2017 Department of Defense – Allied Nations Technical Corrosion Conference. Birmingham, AL.
Justin W. Rausch, Sarah E. Galyon-Dorman, and Scott A. Fawaz (2017). Corrosion Fatigue Pit-to-Crack Test Methodology. The 29th Symposium of the International Committee on Aeronautical Fatigue, Nagoya, Japan.
Galyon Dorman, Sarah, Yongwon Lee, Deborah M. Sweeney, Jenifer Warner, Ralph Bush, Scott A. Fawaz (2010). Environmental Fatigue Crack Propagation in AA 7075-T651. Proceedings of the 2010 Aircraft Airworthiness & Sustainment Conference, Austin, TX.
Galyon Dorman, Sarah E., James Greer, Scott Fawaz, Herve Chevalier, Monica Poelking (2010). 3-D Crack Growth and Residual Strength in Titanium. Proceedings of the 2010 Aircraft Airworthiness & Sustainment Conference, Austin, TX.
Galyon, Sarah E., Saravanan R. Arunachalam, James Greer, Matthew Hammond, and Scott A. Fawaz (2009). Three Dimensional Crack Growth Prediction. The 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, NL.
Hill, Daniel, and Scott A. Fawaz (2009). Validation of Stress Intensity Factors. The 11th Joint FAA/NASA/DOD Conference on Aging Aircraft, Kansas City, MO.
Galyon, Sarah E., James Greer, Saravanan R. Arunachalam, Matthew Hammond, and Scott Fawaz (2009). 3D Crack Growth and Residual Strength. The 11th Joint FAA/NASA/DOD Conference on Aging Aircraft, Kansas City, MO.
Walters, M. R., Sandeep Shah, and S. A. Fawaz (2007). SCC in AA7079-T6 Fuselage Skin Panels. The 9th Joint FAA/NASA/DOD Conference on Aging Aircraft, Palm Springs, CA.
Verhoeven, S., C. Guijt, and S. Fawaz (2005). Bonded Repair of Exfoliation Corrosion. The 8th Joint DOD/FAA/NASA Conference on Aging Aircraft, Palm Springs.
Andersson, B. and S. A. Fawaz. (2004). Statistical Fatigue and Residual Strength Analysis of New/Aging Aircraft Structures. High Performance Computing User Group Conference, Williamsburg, VA.
de Rijck, J. J. M. and S. A. Fawaz. (2000). A Simplified Approach for Stress Analysis of Mechanically Fastened Joints (Text, Figures). 4th Joint DOD/FAA/NASA Conference on Aging Aircraft, St. Louis, MO.
de Rijck, R., S. A. Fawaz, J. Schijve, and A. Vlot (1999). Stress Intensity Factors and Crack Interaction of Part-Elliptical Through Cracks in Adjacent Holes (Text, Figures). 20th Symposium of the International Committee on Aeronautical Fatigue, Bellevue, WA, EPIC.
Fawaz, S. A., J. Schijve, and A. U. de Koning (1997). Fatigue Crack Growth in Riveted Lap Splice Joints. 19th Symposium of the International Committee on Aeronautical fatigue, Edinburgh, Scotland, EMAS/SoMat Systems International Ltd.