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Brian E. Smith
Phone: 650-604-6669
E-Mail: Brian Smith
Curriculum Vitae  (click to expand/minimize)
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(2008)  NASA Group Achievement Award, NAOMS Information Release Team
(2003)  Technology Turning Goals Into Reality (TGIR) Awards, Performance Data Analysis and Reporting System (PDARS)
(1999)  Tech Brief Award, Secondary wing system for use on an aircraft
(1998)  Special Act Award, Special Act Award for liaison role in Coherent Analytical Computing Environment (CASE) Marine Corps AV-8B Harrier Flight Safety Program
(1997)  Superior Accomplishment Award, Commendation letter from High Speed Research (HSR) Program Aerodynamics Performance Technology Manager for leadership of design and testing of the 5% Technology Concept HSR model in the Langley 14- by 22-Foot Wind Tunnel
(1996)  Special Act Award, Special Act Award for 4EPIC (4-Engine Propulsion Integration Concept) advocacy
(1995)  Ames Group Achievement Award, High-lift Engine Aeroacoustics Technology (HEAT) test
(1994)  Special Act Award, Testing of the HSR 2.2% Arrow Wing model in the Ames 12-Foot Pressure Tunnel and the 13.5% HEAT model in the 40- by 80-Foot Wind Tunnel
(1992)  Armed Forces, Letter of appreciation from Naval Air Warfare Center for BOA-1M missile test team
(1991)  Ames Group Achievement Award, Short Takeoff Vertical Landing (STOVL) E- 7A full-scale research program
(1989)  Ames Group Achievement Award, National Full-scale Aerodynamic Complex (NFAC) Integrated Systems Test
(1989)  Special Act Award, National Full-scale Aerodynamic Complex (NFAC) Integrated Systems Test
(1989)  Special Act Award, Identifying potentially catastrophic safety problem with 80- by 120-Foot Wind Tunnel
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PDF download  J. M. Feldman, I. . Barshi, B. E. Smith, & B. . Matthews (2021) Reports of resilient performance: Investigating operators’ descriptions of safety-producing behaviors in the ASRS, In Proceedings of the 2021 International Symposium on Aviation Psychology Virtual Conference Click to read more
PDF download  J. B. Holbrook, M. . Stewart, B. E. Smith, L. J. Prinzel, B. . Matthews, I. . Avrekh, C. . Cardoza, O. . Ammann, V. . Adduru, & C. H. Null (2019) Human Performance Contributions to Safety in Commercial Aviation, NASA/TM-2019-220417 Click to read more
B. E. Smith, M. . Clark, R. . den Hertog, M. . Kavoliunas, & A. . Marosvari (2011) Predicting Future Aviation Safety Issues using a Data-driven Process, 29th International Systems Safety Conference, Las Vegas, NV, 8-12 August 2011 Click to read more
B. E. Smith (2009) Prognostic Aviation Safety in the 21st Century - The Future Aviation Safety Team, International System Safety Conference, Baltimore, MD, August 2009 Click to read more
B. E. Smith, H. D. Jong, & M. H. Everdij (2008) A Prognostic Method to Identify Hazards for Future Aviation, 26th International Congress of the Aeronautical Sciences, Anchorage, Alaska, September 14-19, 2008. Click to read more
B. E. Smith (2007) Prognostic Aviation Safety in the 21st Century - The Future Aviation Safety Team, Smith, B.E., "Prognostic Aviation Safety in the 21st Century- The Future Aviation Safety Team", 21st International System Safety Conference, August 13-17, 2007, Baltimore, MD. Click to read more
B. E. Smith (2007) System Safety & Reliability of Current Modern Large Jet Aircraft. Click to read more
B. E. Smith, & T. . Porter (2005) FAST Hazard Identification and Management Process - an ATM and Airborne Case Study, Smith, B. and Porter, T. (2005), FAST Hazard Identification and Management Process - an ATM and Airborne Case Study. Clinics Session 2, CAATS Safety R&D Workshop, 18-20 October 2005, EUROCONTROL HQ, Brussels. Click to read more
F. A. Zuniga, & B. E. Smith (1997) High-Lift Engine Aeroacoustics Technology (HEAT) Overview, Zuniga, F.A, and Smith, B.E., "High-Lift Engine Aeroacoustics Technology (HEAT) Overview", High-Speed Research Program Aerodynamic Performance Technology Workshop, NASA Langley Research Center, Hampton, Virginia, February 25-28, 1997. Click to read more
S. M. Jaeger, & B. E. Smith (1996) Acoustic Measurements of a Model Semi-Span Symmetry Plane, Jaeger, S.M, Smith, B.E., "Acoustic Measurements of a Model Semi-Span Symmetry Plane", AIAA/CAES Paper 96-1715, 2nd AIAA/CAES Aeroacoustics Conference, State College, Pennsylvania, May 6-8, 1996. Click to read more
B. E. Smith (1996) Net Propulsive Forces Generated by the Integrated HEAT Configuration, Smith, B.E., "Net Propulsive Forces Generated by the Integrated HEAT Configuration", High-Speed Research Program High-Lift Engine Aeroacoustics Technology Workshop, NASA Ames Research Center, March 5-7, 1996. Click to read more
B. E. Smith (1996) Overview and Background of Test Objectives, Smith, B.E., "Overview and Background of Test Objectives", High-Speed Research Program High-Lift Engine Aeroacoustics Technology Workshop, NASA Ames Research Center, March 5-7, 1996. Click to read more
B. E. Smith (1996) Propulsion-Induced Aerodynamic Effects Measured with a 13.5% HSCT Model, Smith, B.E., "Propulsion-Induced Aerodynamic Effects Measured with a 13.5% HSCT Model", High-Speed Research Program High-Lift Engine Aeroacoustics Technology Workshop, NASA Ames Research Center, March 5-7, 1996. Click to read more
B. E. Smith, P. T. Soderman, & F. A. Zuniga (1996) Summary of HEAT 1 Aeroacoustic Installation Effects, Smith, B.E., Soderman, P.T., and Zuniga, F.A, "Summary of HEAT 1 Aeroacoustic Installation Effects", High-Speed Research Program Configuration Aerodynamics Workshop, NASA Langley Research Center, February 27-29, 1996. Click to read more
B. E. Smith, W. A. Poppen, & J. D. Lye (1994) Propulsion-Induced Aerodynamic Effects Measured with a Full-Scale STOVL Model, Smith, B.E., Poppen, W.A., Lye, J.D., "Propulsion-Induced Aerodynamic Effects Measured with a Full-Scale STOVL Model", AIAA Journal of Aircraft, Vol. 31, No. 2, March-April 1994. Click to read more
B. E. Smith, D. . Garland, & W. A. Poppen (1992) Aerodynamic Performance of a Full-Scale Lifting Ejector System in a STOVL Fighter Aircraft, Smith, B.E., Garland, D., Poppen, W.A., "Aerodynamic Performance of a Full-Scale Lifting Ejector System in a STOVL Fighter Aircraft", AIAA 92-3094 presented at 28th Joint Propulsion Conference, Nashville, TN, July 1992. Click to read more
T. . Naumowicz, & B. E. Smith (1992) Hover Performance Validation of an Ejector-Configured STOVL Fighter Aircraft, Naumowicz, T, and Smith, B.E., "Hover Performance Validation of an Ejector-Configured STOVL Fighter Aircraft", AIAA Paper 92-4255, Presented at AIAA Aircraft Design Systems Meeting, Hilton Head, South Carolina , August 24-26, 1992. Click to read more
W. A. Poppen, B. E. Smith, & J. D. Lye (1991) Propulsion-Induced Aerodynamic Effects Measured with a Full-Scale STOVL Model, Poppen, W.A., Smith, B.E., Lye, J.D., "Propulsion-Induced Aerodynamic Effects Measured with a Full-Scale STOVL Model", AIAA Paper 91-0765, Presented at AIAA 29th Aerospace Sciences Meeting, Reno, NV, January 7-10, 1991. Click to read more
B. E. Smith (1990) Aerodynamics of a Lifting Ejector in a STOVL Fighter Aircraft, Smith, B.E., " Aerodynamics of a Lifting Ejector in a STOVL Fighter Aircraft", Oral Presentation at SAE Aerospace Atlantic, Dayton, Ohio, April 24-26, 1990. Click to read more
B. E. Smith, P. T. Zell, & P. M. Shinoda (1990) Comparison of Model and Full-Scale Wind Tunnel Performance, Smith, B. E., Zell, P. T. , and Shinoda, P. M., "Comparison of Model and Full-Scale Wind Tunnel Performance", AIAA Journal of Aircraft, Vol. 27, No. 3, March 1990. Click to read more
M. D. Dudley, B. E. Smith, V. . Corsiglia, & D. L. Ashby (1990) Large-Scale Wind Tunnel Studies of a Jet-Engine Powered Ejector-Lift STOVL Aircraft, Dudley, M.R., Smith, B.E., Corsiglia, V., Ashby, D.L, "Large-Scale Wind Tunnel Studies of a Jet-Engine Powered Ejector-Lift STOVL Aircraft", Paper III.1, Presented at the International Powered-Lift Conference, London, August 29-31, 1990. Click to read more
M. D. Dudley, B. E. Smith, V. . Corsiglia, & D. L. Ashby (1990) Large-Scale Wind Tunnel Studies of a Jet-Engine Powered Ejector-Lift STOVL Aircraft, Dudley, M.R., Smith, B.E., Corsiglia, V., Ashby, D.L, "Large-Scale Wind Tunnel Studies of a Jet-Engine Powered Ejector-Lift STOVL Aircraft", A-90-46-127-1000, Presented at the 46th Annual Forum of the American Helicopter Society, May 21-23, 1990. Click to read more
B. E. Smith, & M. D. Dudley (1989) Aerodynamic Performance of an Ejector System Integrated into a STOVL Aircraft, Smith, B.E. and Dudley, M.D., "Aerodynamic Performance of an Ejector System Integrated into a STOVL Aircraft", Oral Presentation at SAE Aerotech '89, Anaheim, California, September 25-28, 1989. Click to read more
V. . Corsiglia, J. . Farbridge, M. D. Dudley, & B. E. Smith (1989) Large-Scale Wind Tunnel Tests of an Ejector-Lift STOVL Aircraft Model, Corsiglia, V.R., Farbridge, J., Dudley, M.D., and Smith, B.E., "Large-Scale Wind Tunnel Tests of an Ejector-Lift STOVL Aircraft Model", AIAA Paper 89-2905, Presented at AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, Monterey, California, July 10-12, 1989. Click to read more
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Last Updated: May 19, 2020