Jeffrey P. Thomas

Thomas Lord Department of Mechanical Engineering and Materials Science

Assistant Research Professor in the Thomas Lord Department of Mechanical Engineering and Materials Science

Jeffrey P. Thomas Profile Photo

Research Themes

Aerodynamics & Aeroelasticity

Bio

Dr. Thomas' field of research is computational aeroelasticity. This is the study of fluid and structural interaction. Dr. Thomas develops numerical methods to simulate complex physical phenomena.

Education

B.S. University of Kansas, 1989
M.S. University of Kansas, 1991
Ph.D. University of Michigan, Ann Arbor, 1996

Positions

Assistant Research Professor in the Thomas Lord Department of Mechanical Engineering and Materials Science

Courses Taught

ME 639: Computational Fluid Mechanics and Heat Transfer
ME 555: Advanced Topics in Mechanical Engineering
ME 491: Special Projects in Mechanical Engineering
ME 490: Special Topics in Mechanical Engineering
ME 472: Aircraft Performance

Publications

Thomas JP, Dowell EH. Methodology for Numerically Stabilizing a Harmonic-Balance-Based Forced Response Aeroelastic Solution Approach. AIAA Journal. 2023 Feb 1;61(2):965–72.
Thomas JP, Dowell EH. Using Broyden’s Method to Improve the Computational Performance of a Harmonic Balance Aeroelastic Solution Technique. In: AIAA SciTech Forum and Exposition, 2023. 2023.
Brown C, McGowan G, Cooley K, Deese J, Josey T, Dowell EH, et al. Convolution/Volterra Reduced-Order Modeling for Nonlinear Aeroelastic Limit Cycle Oscillation Analysis and Control. AIAA Journal. 2022 Dec 1;60(12):6647–64.
Brown C, McGowan G, Cooley K, Deese J, Josey T, Dowell EH, et al. Convolution/Volterra Reduced-Order Modeling for Flutter and LCO Predictions in Highly Nonlinear Systems. In: AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. 2022.
Thomas JP, Dowell EH. Non-Intrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification. In: AIAA AVIATION 2022 Forum. 2022.
Thomas JP, Dowell EH. Nonlinear Aeroelastic Reduced-Order Modeling Approach with Geometric Gradient Computation Capability. In: AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021. 2021.
Thomas JP, Dowell EH. Automatic differentiation based nonlinear reduced-order model with geometric gradient computation capability. In: AIAA Scitech 2021 Forum. 2021. p. 1–17.
Thomas JP, Dowell EH. Methodology for numerically stabilizing a harmonic balance based aeroelastic solution approach. In: AIAA Scitech 2020 Forum. 2020.
Thomas JP, Dowell EH. Discrete adjoint constrained design optimization approach for unsteady transonic aeroelasticity and buffet. In: AIAA AVIATION 2020 FORUM. 2020. p. 1–13.
Thomas JP, Dowell EH, Anderson M, McGowan GZ. Progress toward efficient compression algorithms for application in flight simulation environments. In: Journal of Aerospace Information Systems. 2019. p. 278–88.
Thomas JP, Dowell EH. Discrete adjoint approach for nonlinear unsteady aeroelastic design optimization. AIAA Journal. 2019 Jan 1;57(10):4368–76.
Kim T, Thomas JP, Dowell EH. Flutter prediction based on dynamic eigen decomposition of coupled CFD-CSD flight simulation. In: International Forum on Aeroelasticity and Structural Dynamics 2019, IFASD 2019. 2019.
Kim T, Thomas JP, Dowell EH. Flutter prediction based on dynamic eigen decomposition of coupled CFD-CSD flight simulation. In: International Forum on Aeroelasticity and Structural Dynamics 2019, IFASD 2019. 2019.
Howison J, Thomas J, Ekici K. Aeroelastic analysis of a wind turbine blade using the harmonic balance method. Wind Energy. 2018 Apr 1;21(4):226–41.
Thomas JP, Dowell EH, Anderson M, McGowan GZ. Progress toward efficient compression algorithms for application in flight simulation environments. In: 2018 Modeling and Simulation Technologies Conference. 2018.
Thomas JP, Dowell EH. A fixed point iteration approach for harmonic balance based aeroelastic computations. In: AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018. 2018.
Besem FM, Thomas JP, Kielb RE, Dowell EH. An aeroelastic model for vortex-induced vibrating cylinders subject to frequency lock-in. Journal of Fluids and Structures. 2016 Feb 1;61:42–59.
Padmanabhan MA, Dowell EH, Thomas JP, Pasiliao CL. Store-induced limit-cycle oscillations due to nonlinear wing-store attachment. Journal of Aircraft. 2016 Jan 1;53(3):778–89.
Besem FM, Kamrass JD, Thomas JP, Tang D, Kielb RE. Vortex-Induced Vibration and Frequency Lock-In of an Airfoil at High Angles of Attack. Journal of Fluids Engineering, Transactions of the ASME. 2016 Jan 1;138(1).
Clark ST, Besem FM, Kielb RE, Thomas JP. Developing a reduced-order model of nonsynchronous vibration in turbomachinery using proper-orthogonal decomposition methods. Journal of Engineering for Gas Turbines and Power. 2015 May 1;137(5).
Thomas JP, Dowell EH. Discrete adjoint design optimization approach for increasing transonic buffet onset angle-of-attack. In: 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2015.
Howison J, Thomas JP, Ekici K. Progress on a wind turbine aeroelastic solution methodology using harmonic balance. In: 33rd Wind Energy Symposium. 2015.
Thomas JP, Dowell EH. Discrete adjoint design optimization approach for increasing transonic buffet onset angle-of-attack. In: 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2015.
Thomas JP, Dowell EH. Discrete adjoint approach for aeroelastic design optimization. In: AIAA AVIATION 2014 -15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2014.
Besem FM, Kamrass JD, Thomas JP, Tang D, Kielb RE. Vortex-induced vibration and frequency lock-in of an airfoil at high angles of attack. In: Proceedings of the ASME Turbo Expo. 2014.
Clark ST, Besem FM, Kielb RE, Thomas JP. Developing a reduced-order model of non-synchronous vibration in turbomachinery using proper-orthogonal decomposition methods. In: Proceedings of the ASME Turbo Expo. 2014.
Thomas JP, Dowell EH, Hall KC. Discrete adjoint method for nonlinear aeroelastic sensitivities for compressible and viscous flows. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2013.
Thomas JP, Dowell EH, Hall KC. Discrete adjoint method for nonlinear aeroelastic sensitivities for compressible and viscous flows. In: 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2013.
Thomas JP, Custer CH, Dowell EH, Hall KC, Corre C. Compact implementation strategy for a harmonic balance method within implicit flow solvers. AIAA Journal. 2013 Jun 1;51(6):1374–81.
Ekici K, Hall KC, Huang H, Thomas JP. Stabilization of explicit flow solvers using a proper-orthogonal- decomposition technique. In: AIAA Journal. 2013. p. 1095–104.
Hall KC, Ekici K, Thomas JP, Dowell EH. Harmonic balance methods applied to computational fluid dynamics problems. International Journal of Computational Fluid Dynamics. 2013 Feb 1;27(2):52–67.
Ekici K, Hall KC, Huang H. Stabilization of explicit flow solvers using a proper orthogonal decomposition technique. In: 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2012.
Thomas JP, Dowell EH, Hall KC. An automatic differentiation based nonlinear reduced order modeling technique for unsteady separated flows. In: 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2012.
Thomas JP, Dowell EH. Airfoil transonic flow buffet calculations using the OVERFLOW 2 flow solver. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2011 Dec 1;
Thomas JP, Léonard. O. Toward a high order throughflow - investigation of the nonlinear harmonic method coupled with an immersed boundary method for the modeling of the circumferential stresses. Journal of Turbomachinery. 2011 May 31;134(1).
Thomas JP, Custer CH, Dowell EH, Hall KC. F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2010.
Thomas JP, Léonard O. Towards a high order throughflow. Part I: Investigating the effectiveness of a harmonic reconstruction for 3D flows. In: Proceedings of the ASME Turbo Expo. 2010. p. 831–41.
Thomas JP, Léonard O. Towards a high order throughflow. Part II: Investigation of the nonlinear harmonic method coupled with an immersed boundary method for the modeling of the circumferential stresses. In: Proceedings of the ASME Turbo Expo. 2010. p. 843–53.
Thomas JP, Dowell EH, Hall KC. Using automatic differentiation to create a nonlinear reduced-order-model aerodynamic solver. AIAA Journal. 2010 Jan 1;48(1):19–24.
Meingast M, Kielb RE, Thomas JP. Preliminary flutter design method for supersonic low pressure turbines. Proceedings of the ASME Turbo Expo. 2009 Dec 1;6(PART A):507–15.
Simon JF, Thomas JP, Léonard O. On the role of the deterministic and circumferential stresses in throughflow calculations. Journal of Turbomachinery. 2009 Jul 1;131(3).
Ortner K, Kohns A, Turley F, Thomas J. Erosion Resistant Coatings for Aircraft Engines. Vakuum in Forschung und Praxis. 2009 Jun 1;21(3):18–21.
Léonard O, Thomas JP, Borguet S. Ten years of experience with a small jet engine as a support for education. Journal of Engineering for Gas Turbines and Power. 2009 Jan 1;131(1).
Spiker MA, Kielb RE, Thomas JP, Hall KC. Application of enforced motion to study 2-D cascade lock-in effect. In: 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2009.
Thomas JP, Custer CH, Dowell EH, Hall KC. Unsteady flow computation using a harmonic balance approach implemented about the OVERFLOW 2 flow solver. In: 19th AIAA Computational Fluid Dynamics Conference. 2009.
Schwarz JB, Dowell EH, Thomas JP, Hall KC, Rausch RD, Bartels RE. Improved flutter boundary prediction for an isolated two-degree-of-freedom airfoil. Journal of Aircraft. 2009 Jan 1;46(6):2069–76.
Dowell EH, Thomas JP, Hall KC, Denegri CM. Theoretical predictions of F-16 fighter limit cycle oscillations for flight flutter testing. Journal of Aircraft. 2009 Jan 1;46(5):1667–72.
Dowell EH, Hall KC, Thomas JP, Kielb RE, Spiker MA, Li A, et al. Reduced order models in unsteady aerodynamic models, aeroelasticity and molecular dynamics. In: ICAS Secretariat - 26th Congress of International Council of the Aeronautical Sciences 2008, ICAS 2008. 2008. p. 4002–14.
Thomas JP, Léonard O. Investigating circumferential non-uniformities in throughflow calculations using an harmonic reconstruction. In: Proceedings of the ASME Turbo Expo. 2008. p. 2229–41.
Spiker MA, Kielb RE, Hall KC, Thomas JP. Efficient design method for non-synchronous vibrations using enforced motion. In: Proceedings of the ASME Turbo Expo. 2008. p. 735–47.
Léonard O, Thomas JP, Borguet S. Ten years of experience with a small jet engine as a support for education. In: Proceedings of the ASME Turbo Expo. 2008. p. 11–21.
Dowell EH, Hall KC, Thomas JP, Kielb RE, Spiker MA, Denegri CM. A new solution method for unsteady flows around oscillating bluff bodies. Solid Mechanics and its Applications. 2008 Jan 1;8:37–44.
Bakhle MA, Thomas JP, Reddy TSR. Fan flutter computations using the harmonic balance method. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 2008 Jan 1;
Thomas JP, Dowels EH, Hall KC, Denegri CM. Virtual aeroelastic flight testing for the F-16 fighter with stores. In: Collection of Technical Papers - US Air Force T and E Days, 2007(Test and Evaluation. 2007. p. 339–46.
Liu L, Dowell EH, Thomas JP. A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces. Journal of Fluids and Structures. 2007 Apr 1;23(3):351–63.
Thomas JP, Dowell EH, Hall KC, Denegri CM. An investigation of the sensitivity of F-16 fighter flutter onset and limit cycle oscillations to uncertainties. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2006. p. 3137–44.
Attar PJ, Dowell EH, White JR, Thomas JP. Reduced order nonlinear system identification methodology. AIAA Journal. 2006 Aug 1;44(8):1895–904.
Thomas JP, Dowell EH, Hall KC. Using automatic differentiation to create a nonlinear reduced order model of a computational fluid dynamic solver. In: Collection of Technical Papers - 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2006. p. 2437–49.
Liu L, Thomas JP, Dowell EH, Attar P, Hall KC. A comparison of classical and high dimensional harmonic balance approaches for a Duffing oscillator. J Comput Phys (USA). 2006;215(1):298–320.
Spiker MA, Thomas JP, Hall KC, Kielb RE, Dowell EH. Modeling cylinder flow vortex shedding with enforced motion using a harmonic balance approach. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2006. p. 4549–58.
Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics. Journal of Aircraft. 2006;43(4):865–78.
Thomas JP, Dowell EH, Hall KC, Denegri CM. Further investigation of modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2005. p. 1457–66.
Dowell EH, Hall KC, Thomas JP, Kielb RE, Spiker MA, Denegri CM. Reduced order unsteady aerodynamic models and aeroelasticity. In: 12th International Congress on Sound and Vibration 2005, ICSV 2005. 2005. p. 47–64.
Hall KC, Kielb RE, Ekici K, Thomas JP, Clark WS. Recent advancements in turbomachinery aeroelastic design analysis. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers. 2005. p. 11253–74.
Liu L, Dowell EH, Thomas JP. Higher order harmonic balance analysis for limit cycle oscillations in an airfoil with cubic restoring forces. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2005 Jan 1;3:1467–76.
Carlson HA, Feng JQ, Thomas JP, Kielb RE, Hall KC, Dowell EH. Computational models for nonlinear aeroelasticity. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers. 2005. p. 4143–52.
Thomas Jeffrey P, Hall Kenneth C, Dowell Earl H. Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities. AIAA Journal. 2005;43(9):1931–6.
Thomas JP, Dowell EH, Hall KC, Denegri CM. Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2004. p. 2044–50.
Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach. Journal of Aircraft. 2004;41(6):1266–74.
Kholodar Denis B, Dowell Earl H, Thomas Jeffrey P, Hall Kenneth C. Limit-cycle oscillations of a typical airfoil in transonic flow. Journal of Aircraft. 2004;41(5):1067–72.
Dowell EH, Thomas JP, Hall KC. Transonic limit cycle oscillation analysis using reduced order aerodynamic models. Journal of Fluids and Structures. 2004;18(SUPPL):17–27.
Kholodar Denis B, Dowell Earl H, Thomas Jeffrey P, Hall Kenneth C. Improved understanding of transonic flutter: A three-parameter flutter surface. Journal of Aircraft. 2004;41(4):911–7.
Thomas JP, Hall KC, Dowell EH. A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow. In: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2003.
Hall KC, Thomas JP, Ekici K, Voytovych DM. Frequency domain techniques for complex and nonlinear flows in turbomachinery. In: 33rd AIAA Fluid Dynamics Conference and Exhibit. 2003.
Thomas JP, Hall KC, Dowell EH. A discrete adjoint approach for modeling unsteady aerodynamic design sensitivities. In: 41st Aerospace Sciences Meeting and Exhibit. 2003.
Thomas JP, Dowell EH, Hall KC. Modeling limit cycle oscillations for an NLR 7301 airfoil aeroelastic configuration including correlation with experiment. In: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2003.
Thomas JP, Hall KC, Dowell EH. A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2003. p. 4779–84.
Thomas JP, Dowell EH, Hall KC. Modeling limit cycle oscillations for an NLR 7301 airfoil aeroelastic configuration including correlation with experiment. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2003. p. 289–97.
Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Three-dimensional transonic aeroelasticity using proper orthogonal decomposition-based reduced-order models. Journal of Aircraft. 2003;40(3):544–51.
Thomas JP, Hall KC, Dowell EH. A discrete adjoint approach for modeling unsteady aerodynamic design sensitivities. In: 41st Aerospace Sciences Meeting and Exhibit. 2003.
Kholodar Denis B, Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Parametric study of flutter for an airfoil in inviscid transonic flow. Journal of Aircraft. 2003;40(2):303–13.
Thomas JP, Hall KC, Dowell EH. A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow. In: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2003.
Kielb Robert E, Thomas Jeffrey P, Barter John W, Hall Kenneth C. Blade excitation by aerodynamic instabilities - A compressor blade study. In: American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI. 2003. p. 399–406.
Kholodar DB, Thomas JP, Dowell EH, Hall KC. A parameter study of transonic airfoil flutter and limit cycle oscillation behavior. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2002. p. 64–79.
Thomas JP, Dowell EH, Hall KC. Modeling viscous transonic limit cycle oscillation behavior using a harmonic balance approach. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2002. p. 1658–66.
Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations. AIAA Journal. 2002;40(4):638–46.
Hall Kenneth C, Thomas Jeffrey P, Clark WS. Computation of unsteady nonlinear flows in cascades using a harmonic balance technique. AIAA Journal. 2002;40(5):879–86.
Thomas JP, Dowell EH, Hall KC. A harmonic balance approach for modeling three-dimensional nonlinear unsteady aerodynamics and aeroelasticity. In: ASME International Mechanical Engineering Congress and Exposition, Proceedings. 2002. p. 1323–34.
Thomas JP, Dowell EH, Hall KC. Three-Dimensional transonic Aeroelasticity using proper orthogonal decomposition based reduced order models. In: 19th AIAA Applied Aerodynamics Conference. 2001.
Thomas JP, Dowell EH, Hall KC. Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations. In: 19th AIAA Applied Aerodynamics Conference. 2001.
Dowell EH, Thomas JP, Hall KC. Transonic limit cycle oscillation analysis using reduced order aerodynamic models. In: 19th AIAA Applied Aerodynamics Conference. 2001.
Thomas JP, Dowell EH, Hall KC. A static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics. In: 39th Aerospace Sciences Meeting and Exhibit. 2001.
Thomas JP, Dowell EH, Hall KC. A static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics. In: 39th Aerospace Sciences Meeting and Exhibit. 2001.
Thomas JP, Dowell EH, Hall KC. Three-Dimensional transonic Aeroelasticity using proper orthogonal decomposition based reduced order models. In: 19th AIAA Applied Aerodynamics Conference. 2001.
Thomas JP, Dowell EH, Hall KC. Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations. In: 19th AIAA Applied Aerodynamics Conference. 2001.
Thomas JP, Dowell EH, Hall KC. Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2001. p. 230–41.
Dowell EH, Thomas JP, Hall KC. Transonic limit cycle oscillation analysis using reduced order aerodynamic models. In: 19th AIAA Applied Aerodynamics Conference. 2001.
Dowell EH, Thomas JP, Hall KC. Transonic limit cycle oscillation analysis using reduced order aerodynamic models. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2001. p. 255–63.
Thomas JP, Dowell EH, Hall KC. Three-dimensional transonic aeroelasticity using proper orthogonal decomposition based reduced order models. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2001. p. 2555–64.
Hall Kenneth C, Thomas Jeffrey P, Dowell Earl H. Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows. AIAA Journal. 2000;38(10):1853–62.
Hall KC, Thomas JP, Dowell EH. Reduced-order modelling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique. In: 37th Aerospace Sciences Meeting and Exhibit. 1999.
Hall KC, Thomas JP, Dowell EH. Reduced-order modelling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique. In: 37th Aerospace Sciences Meeting and Exhibit. 1999.
Dowell EH, Hall KC, Thomas JP, Florea R, Epureanu BI, Heeg J. Reduced order models in unsteady aerodynamics. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 1999. p. 622–37.
Kirn C, Roe PL, Thomas JP. Accurate schemes for advection and aeroacoustics. In: 13th Computational Fluid Dynamics Conference. 1997. p. 47–57.
Kirn C, Roe PL, Thomas JP. Accurate schemes for advection and aeroacoustics. In: 13th Computational Fluid Dynamics Conference. 1997. p. 47–57.
Thomas JP, Kim C, Roe PL. Progress towards a new computational scheme for aeroacoustics. In: 12th Computational Fluid Dynamics Conference. 1995. p. 1325–38.
Thomas JP, Kim C, Roe PL. Progress towards a new computational scheme for aeroacoustics. In: 12th Computational Fluid Dynamics Conference. 1995. p. 1325–38.
Thomas JP, Roe PL. Development of non-dissipative numerical schemes for computational aeroacoustics. In: 11th Computational Fluid Dynamics Conference, 1993. 1993. p. 906–16.