Brian Kestner
Dr. Brian Kestner
Research Engineer II
Weber, Rm 308
(404) 305 - 2781
brian.kestner (at) asdl.gatech.edu
Education
- Bachelor of Science in Mechanical Engineering, Milwaukee School of Engineering, May 1998
- Master of Science in Mechanical Engineering, University of Wisconsin, May 2001
- Doctor of Philosophy in Aerospace Engineering, Georgia Institute of Technology, December 2009
Research
- Technology assessment for N+2 Tube-and-Wing and Hybrid-Wing_Body configurations for simultaneous fuel burn, noise, and emissions reduction. Research sponsored by NASA Integrated System Research Program, Environmentally Responsible Aviation (ERA) project.
- Transient and real-time simulation of combined cycle power plants
- Airframe and mission analysis using NPSS
- Dynamic simulation in NPSS using a volume dynamics approach
- Transient gas turbine simulation using surrogate models
- Gas turbine gas path diagnostics using Bayesian inference networks
- Gas turbine performance anomaly detection using Kalman filters
- Parametric design space exploration of variable cycle engine for supersonic business jet application
Honors and Distinctions
- NASA University Research Engineering Technology Institute (URETI) on Aeropropulsion and Power Technology (UAPT) award for “Outstanding Doctoral Student”.
Membership and Service
- Member, American Institute of Aeronautics and Astronautics, 2009 – Present
Selected Publications
- Kestner, B., Tai, J.C.M., and Mavris, D.N., “Multivariable PI Control for Tip-Jet Reaction Drive Systems”, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, CO: AIAA 2009-4808, 2009
- Kestner, B., Schutte, J., Gladin, J., and Mavris, D.N., ”Ultra High Bypass Ratio Engine sizing and Cycle Selection Study for a Subsonic Commercial Aircraft in the N+2 Timeframe”, Proceedings of ASME Turbo Expo 2011, Vancouver, Canada: GT2011-45370, 2011
- Kestner, B.K., et.al., ” Diagnostics of Highly Degraded Industrial Gas Turbines Using Bayesian Networks”, Proceedings of ASME Turbo Expo 2011, Vancouver, Canada: GT2011-45943, 2011
- Rezvani, R., et. al., “A Gas Turbine Engine Model of Transient Operation Across the Flight Envelope”, Proceedings of ASME Turbo Expo 2011, Vancouver, Canada: GT2011-45565, 2011
- Kestner, B.K., Tai, J.C.M, and Mavris, D.N., “A Computationally Efficient Methodology for Generating Training Data for a Transient Neural Network of a Tip-Jet Reaction Drive System”, To be published in Journal of Engineering for Gas Turbines and Power, GTP-10-1354
