SCOTT
PROST-DOMASKY
Summary
Over twenty-five
years experience in the application of advanced engineering concepts. Twelve
years in the development and applications of finite element methods (FEM/FEA) to
structural analysis of linear and nonlinear mechanical systems: aircraft lap
joints, composite delaminations, orthopedic implants, heart pumps, and blood
cells. Three years experience in aerospace propulsion research and development
for two aircraft manufacturers. Additional experience with biomedical industry
as chief engineer for orthopedic implant manufacturer. A Registered
Professional Engineer in the State of Missouri since 1999.
Present Position:
Structural Analysis Consultant with Analytical Processes / Engineered
Solutions, Inc., St. Louis, MO. Responsibilities consist of development of
stress analysis modeling techniques for corroded aircraft fuselage lap joints,
micro and macro surface profiles, non-aircraft structure including medical
device and metal forming press. Also responsible for writing research grant
proposals, writing technical papers, and preparing conference presentations.
1997 Chief Engineer, Whiteside Biomechanics,
St. Louis, MO
• Designed, developed, and analyzed orthopedic implants for small implant manufacturer
• Supervised staff of six; regulatory, inventory, quality, production
1995
- 1997 Research Associate,
Washington University, St. Louis, MO
• Biochemistry Department: structural analysis using FEM/FEA simulating the nonlinear mechanics of blood tissues
1991
- 1995 Graduate Research Assistant,
Washington University, St. Louis, MO
• Mechanical Engineering Department: structural analysis using FEM/FEA
• Developed FEM computer programs for simulating nonlinear materials—formulated material constitutive laws, verified and validated FEM results against analytical formulas
1989
- 1991 Engineer, Propulsion R&D,
McDonnell Aircraft Co., St. Louis, MO
• Managed cooperative wind tunnel model test program
• Concept development for Advanced Inlet Integration for low observable supersonic fighter aircraft
• Computational, analytical and experimental evaluation of advanced inlet designs.
1988
Graduate Research Assistant,
University of Southern California, LA, CA
• Aerospace Engineering Dept: experimental evaluation of free shear flow fields
1986
- 1987 Associate Engineer, YF-22
Propulsion, Lockheed Aircraft Systems Co., Burbank, CA
• Integrated inlet, nozzle, and engine performance characteristics to evaluate installed engine performance on supersonic fighter
• Performed computational fluid dynamics investigation of nozzle-empennage installation flow fields
1979 - 1987 Airborne Cryptolinguist, US Air Force,
stationed in U.S. and Germany
D.Sc. Mechanical
Engineering, Washington
University, St. Louis, 1995
M.S. Aerospace
Engineering, University of
Southern California, Los Angeles, 1988
B.S. Aerospace
Engineering, University of
Arizona, 1986
Miscellaneous
Structural Mechanics:
Advanced Finite Elements, Continuum Mechanics, Viscoelasticity, Plasticity,
Elasticity, Vibrations, and Energy Methods
Fluid Mechanics:
Advanced Fluid Dynamics, Turbulence, Computational Fluid Dynamics, Gas Dynamics,
Experimental Fluid Mechanics, and Polymer Rheology
Languages:
German spoken. Czech spoken and written.
Computer Languages and Applications: Fortran, Visual Basic, StressCheck, Microsoft Office
Suite.
Professional Associations:
ASTM: Co-chair, Life Methods Task Group, Structural Applications Subcommittee,
Fatigue and Fracture Committee E08.
PUBLICATIONS
1. T. Mills, S. Prost-Domasky, K. Honeycutt, and C. Brooks.
Corrosion and the threat to aircraft structural integrity. In Corrosion Control
in the Aerospace Industry, Woodhead Publishing, 2009.
2. S.A. Prost-Domasky, C.L. Brooks, and N. Young. Verification
of analytical models in a fracture mechanics based approach to modeling
fretting fatigue. In Fatigue and Fracture Mechanics, 35th Volume, ASTM STP
1480, January 2008, 14 pages.
3. S.A. Prost-Domasky, C.L. Brooks, and N. Young. Verification
of analytical models in a fracture mechanics based approach to modeling
fretting fatigue, Journal the ASTM International (Online), Vol. 3, Issue 8,
Sept. 2006, 14 pages.
4. Craig Brooks, Kyle Honeycutt, and Scott Prost-Domasky. Crack
growth and stress intensity prediction techniques. AFRL-VA-WP-TR-2006-3043,
Final Report for 22 April 2002 – 20 March 2006, March 2006. 64 pages.
5. C.L. Brooks, S.A. Prost-Domasky, K.T. Honeycutt, T.B. Mills,
and N. Young. Fretting fatigue model. AFRL-VA-WP-TR-2006-3080, Final Report for
01 May 2003 – 30 April 2006, SBIR Phase II Report, May 2006. 150 pages.
6. S.A. Prost-Domasky, C.L. Brooks, and N. Young. Verification
of analytical models in a fracture mechanics based approach to modeling fretting
fatigue, Journal the ASTM International (Online), Vol. 3, Issue 8, Sept. 2006,
14 pages.
7. Craig Brooks, Kyle Honeycutt, and Scott Prost-Domasky. Crack
growth and stress intensity prediction techniques. AFRL-VA-WP-TR-2006-3043,
Final Report for 22 April 2002 – 20 March 2006, March 2006. 64 pages.
8. C.L. Brooks, S.A. Prost-Domasky, K.T. Honeycutt, T.B. Mills,
and N. Young. Fretting fatigue model. AFRL-VA-WP-TR-2006-3080, Final Report for
01 May 2003 – 30 April 2006, SBIR Phase II Report, May 2006. 150 pages.
9. Craig L. Brooks, Scott A. Prost-Domasky, Kyle T. Honeycutt,
and Thomas B. Mills. Predictive modeling of structure service life. In ASM
Handbook Volume 13A, Corrosion: Fundamental, Testing and Protection, October
2003, 946-958.
10. Scott A. Prost-Domasky, Craig L. Brooks, and Kyle T.
Honeycutt. The application of p-version finite element methods to
fracture-dominated problems encountered in engineering practice. Computer &
Mathematics with Applications (refereed), Vol. 46, No. 1, June 2003, 125-139.
11. C.L. Brooks, S.A. Prost-Domasky, K.T. Honeycutt, T.B. Mills,
and N. Young. Fretting fatigue model. AFRL-VA-WP-TR-2003-3012, Final Report for
01 February 2002 – 30 November 2002, SBIR Phase I Report, February 2003. 55
pages.
12. M. Ulfendahl, E. Chan, W.B. McConnaughey, S. Prost-Domasky,
and E.L. Elson. Measurements of stiffness in isolated inner ear sensory cells.
European Journal of Physiology (refereed), Vol. 436, 1998, 9-15.
13. Scott A. Prost-Domasky, Barna A. Szabó, and George I.
Zahalak. Large-deformation analysis of nonlinear viscoelastic fluids. Computers
and Structures, Vol. 64, No. 5-6, June 1997, 200-220. (error in title)
14. Scott A. Prost-Domasky and Bamin Khomami. A note on start up
and large amplitude oscillatory shear flow of multimode viscoelastic fluids.
Rheologica Acta (refereed), Vol. 35, No. 3, July 1996, 211-224.
15. Scott A. Prost-Domasky. Large indentations of nonlinear
viscoelastic materials, with an application to cell poking. Doctoral
Dissertation, Washington University, June 1995.
16. F.K. Browand and Scott A. Prost-Domasky. Experiment on
pattern evolution in the 2-D mixing layer. In New Trends in Nonlinear Dynamics
and Pattern-Forming Phenomena, edited by P. Coullet and P. Huerre, Plenum Press, New York,
1990.
1. Scott Prost-Domasky and Kyle Honeycutt. Validation of Cold
Working Simulations with Contour Method and Digital Image Correlation
Measurements. Presented at the ASTM Workshop on Verification and Validation of
Solid Mechanics and Life Prediction Software, Phoenix, Arizona, May 2012.
2. S. Prost-Domasky, C. L. Brooks, T. B. Mills, and K.T.
Honeycutt. Incorporating Laser Peening Residual Stress into a Holistic Life
Assessment Approach. Presented at the Eleventh International ASTM/ESIS
Symposium on Fatigue and Fracture Mechanics, Anaheim, California, May, 2011.
3. Craig Brooks, Kyle Honeycutt, Thomas Mills, and Scott
Prost-Domasky. Incorporating Laser Peening Residual Stress into a Holistic Life
Assessment Approach. Proceedings of the 2010 Aircraft Structural Integrity
Program (ASIP) Conference, San Antonio, Texas November 3-December 2 2010.
4. Thomas B. Mills, Kyle T. Honeycutt, Scott A. Prost-Domasky,
and Craig L. Brooks. Corrosion modeling and life prediction supporting
structural prognostic health management. Paper and Presentation at 2007
International Committee of Aeronautical Fatigue (ICAF 2007) Symposium, Naples,
Italy, May 2007.
5. S. Prost-Domasky, C. L. Brooks and N. Young. Verification of
analytical models in a fracture mechanics based approach to modeling fretting
fatigue. Presented at the Fifth International ASTM/ESIS Symposium on Fatigue
and Fracture Mechanics, Reno, Nevada, May 2005.
6. Scott Prost-Domasky, Tom Mills and Eric Tuegel. Integration
of a fracture mechanics-based fretting model into holistic life assessments.
Presented at the International Symposium on Fretting Fatigue 4, Lyon, France,
2004.
7. Craig Brooks, Scott Prost-Domasky, and Eric Tuegel. Sliding
a fretting model into the holistic life assessment methods. Presented at 2003
International Committee of Aeronautical Fatigue (ICAF 2003), Toulouse, France,
May 2003.
8. Kyle T. Honeycutt, Craig L. Brooks, Scott A. Prost-Domasky,
and Thomas B. Mills. Holistic life assessment methods. Presented at the
Canadian Aeronautics and Space Institute 50th AGM and Conference, 16th
Aerospace Structures and Materials Symposium, Montreal, Canada, April 2003.
9. C. Brooks, K. Honeycutt, and S. Prost-Domasky, and N. Young.
Monitoring the robustness of corrosion & fatigue prediction models.
Presented at the 2001 USAF Aircraft Structural Integrity Program Conference,
Williamsburg, Virginia, December 2001.
10. C. Brooks, K. Honeycutt, S. Prost-Domasky, and N. Young.
Using holistic life predictions to focus NDI requirements. Presented at the
2000 USAF Aircraft Structural Integrity Program Conference, San Antonio, Texas,
December 2000.
11. Scott A. Prost-Domasky, Craig L. Brooks, and Kyle T.
Honeycutt. The application of p-version
finite element methods to fracture-dominated problems encountered in
engineering practice. Presented at the p
and hp Finite Element Methods:
Mathematics and Engineering Practice Conference (p-FEM2000), St. Louis,
Missouri, May 2000.
12. C. Brooks, K. Honeycutt, and S. Prost-Domasky. Case studies
for corrosion/fatigue life assessments. Presented at the Fourth Joint
NASA/FAA/DoD Conference on Aging Aircraft, St. Louis, Missouri, May 2000.
13. C. Brooks, K. Honeycutt, and S. Prost-Domasky. Correlation
of life prediction methods with corrosion-related tests. Presented at the 1999
USAF Aircraft Structural Integrity Program Conference, San Antonio, Texas,
November 1999.
14. Craig Brooks, Deb Peeler, Kyle T. Honeycutt, and Scott
Prost-Domasky. Predictive modeling for corrosion management: modeling
fundamentals. Presented at the Third Joint NASA/FAA/DoD Conference on Aging
Aircraft, Albuquerque, New Mexico, September 1999.
15. K. Honeycutt, C.L. Brooks, and S. Prost-Domasky.
ECLIPSE-Environmental and Cyclic Life Interaction Prediction Software.
Presented at the ASM AEROMAT Conference, Dayton, Ohio, June 1999.
16. C.L. Brooks, S. Prost-Domasky, and K. Honeycutt. Determining
the initial quality state for materials. Presented at the 1998 USAF Aircraft
Structural Integrity Program Conference, San Antonio, Texas, December 1998.
17. C.L. Brooks, S. Prost-Domasky, and K. Honeycutt. Corrosion
is a structural and economic problem: transforming metrics to a life prediction
method. Presented at the NATO RTO’s Workshop 2 on Fatigue in the Presence of
Corrosion, Corfu, Greece, October, 1998.
18. A. Kollias, S. Prost-Domasky, and B. Khomami. Transient
shear flows of multimode fluids. Presented at the AIChE 1993 Annual Meeting,
Nov. 1993.
19. F.K. Browand and Scott A. Prost-Domasky. Vortex patterns in
high Reynolds number shear flow. Presented at the 41st Annual Meeting of the
Division of Fluid Dynamics of the American Physical Society, November 1988.
20. F.K. Browand and Scott A. Prost-Domasky. A technique for
acoustic excitation of separated shear flows: preliminary results. Presented at
the International Symposium on Flow-Induced Vibration and Noise, Nov. 1988.