Publications
Selected publications
- Global stability analysis of elastic aircraft in edge-of-the-envelope flow (Journal article - 2023)
- Resolvent analysis of a finite wing in transonic flow (Journal article - 2023)
- Global instability of wing shock-buffet onset (Journal article - 2020)
- Analysis of a civil aircraft wing transonic shock buffet experiment (Journal article - 2020)
- Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration (Journal article - 2017)
- Enabling off-design linearised aerodynamics analysis using Krylov subspace recycling technique (Journal article - 2016)
2024
GAUSSIAN PROCESSES FOR MERGING WATER COLUMN PARAMETERS
BOULTON, F., COLQUITT, D. J., TIMME, S., & WILLIAMS, D. P. (2024, June 17). GAUSSIAN PROCESSES FOR MERGING WATER COLUMN PARAMETERS. In International Conference on Underwater Acoustics 2024. Institute of Acoustics. doi:10.25144/22219
Data Fusion of Wing Pressure Distributions Using Scalable Gaussian Processes
Anhichem, M., Timme, S., Castagna, J., Peace, A. J., & Maina, M. (n.d.). Data Fusion of Wing Pressure Distributions Using Scalable Gaussian Processes. AIAA Journal, 1-16. doi:10.2514/1.j063317
Bayesian Approaches for Efficient and Uncertainty-Aware Prediction of Pressure Distributions
Anhichem, M., Timme, S., Castagna, J., Peace, A., & Maina, M. (2024). Bayesian Approaches for Efficient and Uncertainty-Aware Prediction of Pressure Distributions. In AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2024-0253
2023
Global stability analysis of elastic aircraft in edge-of-the-envelope flow
Houtman, J., & Timme, S. (2023). Global stability analysis of elastic aircraft in edge-of-the-envelope flow. JOURNAL OF FLUID MECHANICS, 967. doi:10.1017/jfm.2023.413
Identifying Active Regions of Finite-Wing Transonic Buffet using Resolvent Method
Houtman, J., Vevek, U. S., & Timme, S. (2023). Identifying Active Regions of Finite-Wing Transonic Buffet using Resolvent Method. In AIAA AVIATION 2023 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2023-3242
Resolvent Analysis using Subspace Algorithms for Aerodynamic Applications
Vevek, U. S., & Timme, S. (2023). Resolvent Analysis using Subspace Algorithms for Aerodynamic Applications. In AIAA AVIATION 2023 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2023-3767
Resolvent analysis of a finite wing in transonic flow
Houtman, J., Timme, S., & Sharma, A. (2023). Resolvent analysis of a finite wing in transonic flow. FLOW, 3. doi:10.1017/flo.2023.8
Transonic Buffet Characteristics Under Conditions of Free and Forced Transition
Moise, P., Zauner, M., Sandham, N. D., Timme, S., & He, W. (2023). Transonic Buffet Characteristics Under Conditions of Free and Forced Transition. AIAA JOURNAL, 61(3), 1061-1076. doi:10.2514/1.J062362
Bespoke Stability Analysis Tool in Next-Generation Computational Fluid Dynamics Solver
Vevek, U. S., Houtman, J., & Timme, S. (n.d.). Bespoke Stability Analysis Tool in Next-Generation Computational Fluid Dynamics Solver. The Aeronautical Journal. doi:10.1017/aer.2023.108
2022
Aerodynamic Data Modelling and Fidelity Definition for Multifidelity Data Fusion
Anhichem, M., Timme, S., Castagna, J., Peace, A. J., & Maina, M. (n.d.). Aerodynamic Data Modelling and Fidelity Definition for Multifidelity Data Fusion. In Royal Aeronautical Society Applied Aerodynamics Conference 2022.
Bespoke Stability Analysis Tool in Next-Generation Computational Fluid Dynamics Solver
Vevek, U. S., Houtman, J., & Timme, S. (2022, September 13). Bespoke Stability Analysis Tool in Next-Generation Computational Fluid Dynamics Solver. In Royal Aeronautical Society Applied Aerodynamics Conference 2022.
Multifidelity Data Fusion Applied to Aircraft Wing Pressure Distribution
Anhichem, M., Timme, S., Castagna, J., Peace, A., & Maina, M. (2022). Multifidelity Data Fusion Applied to Aircraft Wing Pressure Distribution. In AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2022-3526
Resolvent Analysis of Large Aircraft Wings in Edge-of-the-Envelope Transonic Flow
Houtman, J., Timme, S., & Sharma, A. (2022). Resolvent Analysis of Large Aircraft Wings in Edge-of-the-Envelope Transonic Flow. In AIAA SCITECH 2022 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2022-1329
NEXT-GENERATION COMPUTATIONAL FLUID DYNAMICS CAPABILITY FOR AIRCRAFT AEROELASTICITY AND LOADS
Vevek, U. S., Timme, S., Pattinson, J., Stickan, B., & Büchner, A. (2022). NEXT-GENERATION COMPUTATIONAL FLUID DYNAMICS CAPABILITY FOR AIRCRAFT AEROELASTICITY AND LOADS. In Proceedings of the International Forum of Aeroelasticity and Structural Dynamics 2022, IFASD 2022.
2021
Triglobal infinite-wing shock-buffet study
He, W., & Timme, S. (n.d.). Triglobal infinite-wing shock-buffet study. Journal of Fluid Mechanics. doi:10.1017/jfm.2021.678
Aeroelastic Coupling Effects in Globally Unstable Transonic Wing Flow
Belesiotis-Kataras, P., & Timme, S. (2021). Aeroelastic Coupling Effects in Globally Unstable Transonic Wing Flow. In AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2021-0611
Towards Global Stability Analysis of Flexible Aircraft in Edge-of-the-Envelope Flow
Houtman, J., & Timme, S. (2021). Towards Global Stability Analysis of Flexible Aircraft in Edge-of-the-Envelope Flow. In AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2021-0610
2020
Resolvent Analysis of Shock Buffet on Infinite Wings
He, W., & Timme, S. (2020). Resolvent Analysis of Shock Buffet on Infinite Wings. In AIAA AVIATION 2020 FORUM. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2020-2727
Global instability of wing shock-buffet onset
Timme, S. (2020). Global instability of wing shock-buffet onset. JOURNAL OF FLUID MECHANICS, 885. doi:10.1017/jfm.2019.1001
Analysis of a civil aircraft wing transonic shock buffet experiment
Masini, L., Timme, S., & Peace, A. J. (2020). Analysis of a civil aircraft wing transonic shock buffet experiment. Journal of Fluid Mechanics, 884. doi:10.1017/jfm.2019.906
Harmonic Forcing Amplitude Effects in Globally Unstable Transonic Wing Flow
Belesiotis-Kataras, P., & Timme, S. (2020). Harmonic Forcing Amplitude Effects in Globally Unstable Transonic Wing Flow. In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2020-1985
Triglobal Shock Buffet Instability Study on Infinite Wings
He, W., & Timme, S. (2020). Triglobal Shock Buffet Instability Study on Infinite Wings. In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2020-1986
Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment
Masini, L., Timme, S., & Peace, A. J. (2020). Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment. AIAA JOURNAL, 58(10), 4322-4338. doi:10.2514/1.J059219
2019
Reynolds Number Effects on Wing Shock Buffet Unsteadiness
Masini, L., Timme, S., & Peace, A. J. (2019). Reynolds Number Effects on Wing Shock Buffet Unsteadiness. In AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2019-2820
Flexible aircraft gust encounter simulation using subspace projection model reduction
Bekemeyer, P., & Timme, S. (2019). Flexible aircraft gust encounter simulation using subspace projection model reduction. AEROSPACE SCIENCE AND TECHNOLOGY, 86, 805-817. doi:10.1016/j.ast.2019.02.011
Global Shock Buffet Instability on NASA Common Research Model
Timme, S. (2019). Global Shock Buffet Instability on NASA Common Research Model. In AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2019-0037
Investigation into gust load alleviation using computational fluid dynamics
Bekemeyer, P., Thormann, R., & Timme, S. (2019). Investigation into gust load alleviation using computational fluid dynamics. In International Forum on Aeroelasticity and Structural Dynamics 2019, IFASD 2019.
2018
Numerical Study of Incipient Transonic Shock Buffet on Large Civil Aircraft Wings
Belesiotis Kataras, P., & Timme, S. (2018). Numerical Study of Incipient Transonic Shock Buffet on Large Civil Aircraft Wings. In Royal Aeronautical Society 2018 Applied Aerodynamics Conference. Bristol, UK.
Scale-Resolving Simulation of Shock Buffet Onset Physics on a Civil Aircraft Wing
Masini, L., Timme, S., & Peace, A. J. (2018). Scale-Resolving Simulation of Shock Buffet Onset Physics on a Civil Aircraft Wing. In Royal Aeronautical Society 2018 Applied Aerodynamics Conference. Bristol, UK.
Application of Harmonic Balance Method for Non-linear Gust Responses
Thormann, R., & Timme, S. (2018). Application of Harmonic Balance Method for Non-linear Gust Responses. In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2018-1686
2017
Rapid gust response simulation of large civil aircraft using computational fluid dynamics
Bekemeyer, P., Thormann, R., & Timme, S. (2017). Rapid gust response simulation of large civil aircraft using computational fluid dynamics. AERONAUTICAL JOURNAL, 121(1246), 1795-1807. doi:10.1017/aer.2017.104
Efficient aerodynamic derivative calculation in three-dimensional transonic flow
Thormann, R., & Timme, S. (2017). Efficient aerodynamic derivative calculation in three-dimensional transonic flow. AERONAUTICAL JOURNAL, 121(1244), 1464-1478. doi:10.1017/aer.2017.66
Model reduction for flight dynamics simulations using computational fluid dynamics
Pagliuca, G., & Timme, S. (2017). Model reduction for flight dynamics simulations using computational fluid dynamics. AEROSPACE SCIENCE AND TECHNOLOGY, 69, 15-26. doi:10.1016/j.ast.2017.06.013
Wing-body junction optimisation with CAD-based parametrisation including a moving intersection
Xu, S., Timme, S., Mykhaskiv, O., & Mueller, J. -D. (2017). Wing-body junction optimisation with CAD-based parametrisation including a moving intersection. AEROSPACE SCIENCE AND TECHNOLOGY, 68, 543-551. doi:10.1016/j.ast.2017.06.014
Frequency-Domain Gust Response Simulation using Computational Fluid Dynamics
Bekemeyer, P., Thormann, R., & Timme, S. (2017). Frequency-Domain Gust Response Simulation using Computational Fluid Dynamics. AIAA Journal: devoted to aerospace research and development, 55(7), 2174-2185. doi:10.2514/1.J055373
CAD-based shape optimisation of the NASA CRM wing-body intersection using differentiated CAD-kernel
Mykhaskiv, O., Mohanamuraly, P., Mueller, J. -D., Xu, S., & Timme, S. (2017). CAD-based shape optimisation of the NASA CRM wing-body intersection using differentiated CAD-kernel. In 35th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2017-4080
Reduced Order Transonic Aeroelastic Gust Response Simulation of Large Aircraft
Bekemeyer, P., & Timme, S. (2017). Reduced Order Transonic Aeroelastic Gust Response Simulation of Large Aircraft. In 35th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2017-4361
Gust Analysis using Computational Fluid Dynamics Derived Reduced Order Models
Timme, S., Badcock, K. J., & Da Ronch, A. (2017). Gust Analysis using Computational Fluid Dynamics Derived Reduced Order Models. Journal of Fluids and Structures, 71, 116-125. doi:10.1016/j.jfluidstructs.2017.03.004
Robust and efficient adjoint solver for complex flow conditions
Xu, S., & Timme, S. (2017). Robust and efficient adjoint solver for complex flow conditions. COMPUTERS & FLUIDS, 148, 26-38. doi:10.1016/j.compfluid.2017.02.012
Influence of Vane Vortex Generators on Transonic Wing Buffet: Further Analysis of the BUCOLIC Experimental Dataset
Masini, L., Timme, S., Ciarella, A., & Peace, A. (2017). Influence of Vane Vortex Generators on Transonic Wing Buffet: Further Analysis of the BUCOLIC Experimental Dataset. In 52nd 3AF International Conference on Applied Aerodynamics. Lyon, France.
Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration
Sartor, F., & Timme, S. (n.d.). Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration. AIAA Journal, 55(4), 1230-1240. doi:10.2514/1.J055186
Influence of gust modelling on free-flight aerofoils
Thormann, R., Pagliuca, G., & Timme, S. (2017). Influence of gust modelling on free-flight aerofoils. In 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017 Vol. 2017-June.
Model reduction for gust load analysis of free-flying aircraft
Pagliuca, G., Bekemeyer, P., Thormann, R., & Timme, S. (2017). Model reduction for gust load analysis of free-flying aircraft. In 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017 Vol. 2017-June.
2016
Enabling off-design linearised aerodynamics analysis using Krylov subspace recycling technique
Xu, S., Timme, S., & Badcock, K. (2016). Enabling off-design linearised aerodynamics analysis using Krylov subspace recycling technique. Computers & Fluids, 140, 385-396. doi:10.1016/j.compfluid.2016.10.018
Mach Number Effects on Buffeting Flow on a Half Wing-body Configuration
Sartor, F., & Timme, S. (2016). Mach Number Effects on Buffeting Flow on a Half Wing-body Configuration. International Journal of Numerical Methods for Heat and Fluid Flow, 26(7), 2066-2080. doi:10.1108/HFF-07-2015-0283
Efficient Aerodynamic Derivative Calculation in Three-Dimensional Transonic Flow
Thormann, R., & Timme, S. (2016). Efficient Aerodynamic Derivative Calculation in Three-Dimensional Transonic Flow. In Royal Aeronautical Society 2016 Applied Aerodynamics Conference. Bristol.
Rapid Gust Response Simulation of Large Civil Aircraft using Computational Fluid Dynamics
Bekemeyer, P., Thormann, R., & Timme, S. (2016). Rapid Gust Response Simulation of Large Civil Aircraft using Computational Fluid Dynamics. In Royal Aeronautical Society 2016 Applied Aerodynamics Conference. Bristol.
Flight Dynamics Mode Identification and Model Reduction using Computational Fluid Dynamics
Pagliuca, G., & Timme, S. (2016). Flight Dynamics Mode Identification and Model Reduction using Computational Fluid Dynamics. In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2016-3850
Towards Three-Dimensional Global Stability Analysis of Transonic Shock Buffet
Timme, S., & Thormann, R. (2016). Towards Three-Dimensional Global Stability Analysis of Transonic Shock Buffet. In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2016-3848
Nonlinear reduced-order modelling for limit-cycle oscillation analysis
Gai, G., & Timme, S. (2016). Nonlinear reduced-order modelling for limit-cycle oscillation analysis. Nonlinear Dynamics, 84(2), 991-1009. doi:10.1007/s11071-015-2544-9
Reduced Order Gust Response Simulation using Computational Fluid Dynamics
Bekemeyer, P., & Timme, S. (2016). Reduced Order Gust Response Simulation using Computational Fluid Dynamics. In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2016-1485
LINEARISED FREQUENCY DOMAIN GUST ANALYSIS OF LARGE CIVIL AIRCRAFT
Bekemeyer, P., Thormann, R., & Timme, S. (2016). LINEARISED FREQUENCY DOMAIN GUST ANALYSIS OF LARGE CIVIL AIRCRAFT. In Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016) (pp. 7390-7402). Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece. doi:10.7712/100016.2341.5316
REDUCED ORDER MODELLING OF GUST ANALYSIS USING COMPUTATIONAL FLUID DYNAMICS
Thormann, R., Bekemeyer, P., & Timme, S. (2016). REDUCED ORDER MODELLING OF GUST ANALYSIS USING COMPUTATIONAL FLUID DYNAMICS. In Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016) (pp. 7423-7434). Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece. doi:10.7712/100016.2343.5441
Reduced-Order Modelling of Nonlinear Aircraft Structures
Gai, G., Timme, S., & Badcock, K. (2016). Reduced-Order Modelling of Nonlinear Aircraft Structures. In Royal Aeronautical Society 2016 Applied Aerodynamics Conference. Bristol, UK.
2015
Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration
Sartor, F., & Timme, S. (2015). Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration. In 22nd AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2015-2607
Reynolds-Averaged Navier-Stokes Simulations of Shock Buffet on Half Wing-Body Configuration
Sartor, F., & Timme, S. (2015). Reynolds-Averaged Navier-Stokes Simulations of Shock Buffet on Half Wing-Body Configuration. In 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2015-1939
Delayed detached-eddy simulation of shock buffet on half wing-body configuration
Sartor, F., & Timme, S. (2017). Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration. In AIAA JOURNAL Vol. 55 (pp. 1230-1240). doi:10.2514/1.J055186
Krylov subspace recycling for linearised aerodynamics analysis using DLR-TAU
Xu, S., Timme, S., & Badcock, K. J. (2015). Krylov subspace recycling for linearised aerodynamics analysis using DLR-TAU. In International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015.
Passive control of transonic buffet onset on a half wing-body configuration
Timme, S., & Sartor, F. (2015). Passive control of transonic buffet onset on a half wing-body configuration. In International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015.
2013
Model reduction for linear and nonlinear gust loads analysis
Da Ronch, A., Tantaroudas, N. D., Timme, S., & Badcock, K. J. (2013). Model reduction for linear and nonlinear gust loads analysis. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Parallel Semi-Meshless Stencil Selection for Moving Geometry Simulations
Angulo, J., Kennett, D. J., Timme, S., & Badcock, K. J. (2013). Parallel Semi-Meshless Stencil Selection for Moving Geometry Simulations. In 21st AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2013-2854
An implicit meshless method for application in computational fluid dynamics
Kennett, D. J., Timme, S., Angulo, J., & Badcock, K. J. (2013). An implicit meshless method for application in computational fluid dynamics. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 71(8), 1007-1028. doi:10.1002/fld.3698
Solution of linear systems in Fourier-based methods for aircraft applications
McCracken, A., Da Ronch, A., Timme, S., & Badcock, K. J. (2013). Solution of linear systems in Fourier-based methods for aircraft applications. INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 27(2), 79-87. doi:10.1080/10618562.2012.750719
Semi-Meshless Stencil Selection on Three-Dimensional Anisotropic Point Distributions with Parallel Implementation
Kennett, D., Timme, S., Angulo, J., & Badcock, K. (2013). Semi-Meshless Stencil Selection on Three-Dimensional Anisotropic Point Distributions with Parallel Implementation. In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2013-867
Linear reduced order modelling for gust response analysis using the DLR-TAU code
Timme, S., Badcock, K. J., & Da Ronch, A. (2013). Linear reduced order modelling for gust response analysis using the DLR-TAU code. In IFASD 2013 - International Forum on Aeroelasticity and Structural Dynamics.
2012
Accelerating convergence of the CFD Linear Frequency Domain method by a preconditioned linear solver
McCracken, A. J., Timme, S., & Badcock, K. J. (2012). Accelerating convergence of the CFD Linear Frequency Domain method by a preconditioned linear solver. In ECCOMAS 2012 - European Congress on Computational Methods in Applied Sciences and Engineering, e-Book Full Papers (pp. 1280-1290).
Lyapunov inverse iteration for stability analysis using computational fluid dynamics
Timme, S., Badcock, K. J., Wu, M., & Spence, A. (2012). Lyapunov inverse iteration for stability analysis using computational fluid dynamics. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Semi-meshless stencil selection for anisotropic point distributions
Kennett, D. J., Timme, S., Angulo, J., & Badcock, K. J. (2012). Semi-meshless stencil selection for anisotropic point distributions. INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 26(9-10), 463-487. doi:10.1080/10618562.2012.744450
2011
An Implicit Semi-Meshless Scheme with Stencil Selection for Anisotropic Point Distributions
Kennett, D., Timme, S., Angulo, J., & Badcock, K. (2011). An Implicit Semi-Meshless Scheme with Stencil Selection for Anisotropic Point Distributions. In 20th AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2011-3234
Transonic Aeroelastic Instability Searches Using Sampling and Aerodynamic Model Hierarchy
Timme, S., & Badcock, K. J. (2011). Transonic Aeroelastic Instability Searches Using Sampling and Aerodynamic Model Hierarchy. AIAA JOURNAL, 49(6), 1191-1201. doi:10.2514/1.J050509
Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation
Timme, S., Marques, S., & Badcock, K. J. (2011). Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation. AIAA JOURNAL, 49(6), 1202-1213. doi:10.2514/1.J050975
Calculating the Influence of Structural Uncertainty on Aeroelastic Limit Cycle Response
Badcock, K., Timme, S., Marques, S., Khodaparast, H., & Mottershead, J. (2011). Calculating the Influence of Structural Uncertainty on Aeroelastic Limit Cycle Response. In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2011-1741
Transonic aeroelastic simulation for instability searches and uncertainty analysis
Badcock, K. J., Timme, S., Marques, S., Khodaparast, H., Prandina, M., Mottershead, J. E., . . . Woodgate, M. A. (2011). Transonic aeroelastic simulation for instability searches and uncertainty analysis. PROGRESS IN AEROSPACE SCIENCES, 47(5), 392-423. doi:10.1016/j.paerosci.2011.05.002
Updating Computational Aeroelastic Models using Flight Flutter Test Data
S., T., & K. J., B. (2011). Updating Computational Aeroelastic Models using Flight Flutter Test Data. In International Journal of Aerospace and Lightweight Structures (IJALS) - Vol. 01 (pp. 157). Research Publishing Services. doi:10.3850/s2010428611000183
Updating Computational Aeroelastic Models using Flight Flutter Test Data
Timme, S., & Badcock, K. J. (2011). Updating Computational Aeroelastic Models using Flight Flutter Test Data. International Journal of Aerospace and Lightweight Structures, 1(2), 157-178.
2010
Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation
Timme, S., Marques, S., & Badcock, K. (2010). Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation. In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2010-8228
Searching for Transonic Aeroelastic Instability Using an Aerodynamic Model Hierarchy
Timme, S., & Badcock, K. (2010). Searching for Transonic Aeroelastic Instability Using an Aerodynamic Model Hierarchy. In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2010-3048
Applying Interpolation Techniques to Search for Transonic Aeroelastic Instability: ANN vs Kriging
Rampurawala, A., Timme, S., & Badcock, K. J. (2010). Applying Interpolation Techniques to Search for Transonic Aeroelastic Instability: ANN vs Kriging. In RAeS Aerodynamics Conference. Bristol, UK.: Royal Aeronautical Society Aerodynamics Conference.
2009
Oscillatory Behavior of Transonic Aeroelastic Instability Boundaries
Timme, S., & Badcock, K. J. (2009). Oscillatory Behavior of Transonic Aeroelastic Instability Boundaries. AIAA JOURNAL, 47(6), 1590-1592. doi:10.2514/1.40497
2008
Aeroelasticity based on Bifurcation Theory
Timme, S., & Badcock, K. J. (2008). Aeroelasticity based on Bifurcation Theory. In ECCOMAS. Venice, Italy.: 5th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS).