2013
An implicit meshless method for application in computational fluid dynamics (Journal article)
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.3698DOI: 10.1002/fld.3698
Assessment of tabular models using CFD (Conference Paper)
McCracken, A. J., Kennett, D. J., Badcock, K. J., & da Ronch, A. (2013). Assessment of tabular models using CFD. In AIAA Atmospheric Flight Mechanics (AFM) Conference.
Comparison of Adaptive Sampling Methods for Generation of Surrogate Aerodynamic Models (Conference Paper)
Mackman, T. J., Allen, C. B., Ghoreyshi, M., & Badcock, K. J. (2013). Comparison of Adaptive Sampling Methods for Generation of Surrogate Aerodynamic Models. In AIAA Journal Vol. 51 (pp. 797-808). doi:10.2514/1.J051607DOI: 10.2514/1.J051607
Linear reduced order modelling for gust response analysis using the DLR-TAU code (Conference Paper)
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.
Model reduction for linear and nonlinear gust loads analysis (Conference Paper)
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.
Model reduction for linear and nonlinear gust loads analysis (Conference Paper)
Da Ronch, A., Tantaroudas, N. D., Timme, S., & Badcock, K. J. (2013). Model reduction for linear and nonlinear gust loads analysis. In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. doi:10.2514/6.2013-1492DOI: 10.2514/6.2013-1492
Parallel semi-meshless stencil selection for moving geometry simulations (Conference Paper)
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.
Reduction of nonlinear models for control applications (Conference Paper)
Da Ronch, A., Tantaroudas, N. D., & Badcock, K. J. (2013). Reduction of nonlinear models for control applications. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Reduction of nonlinear models for control applications (Conference Paper)
Da Ronch, A., Tantaroudas, N. D., & Badcock, K. J. (2013). Reduction of nonlinear models for control applications. In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. doi:10.2514/6.2013-1491DOI: 10.2514/6.2013-1491
Semi-meshless stencil selection on three-dimensional anisotropic point distributions with parallel implementation (Conference Paper)
Kennett, D. J., Angulo, J., Timme, S., & Badcock, K. J. (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 2013.
Solution of linear systems in Fourier-based methods for aircraft applications (Journal article)
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:10.1080/10618562.2012.750719DOI: 10.1080/10618562.2012.750719
Transonic Aerodynamic Load Modeling of X-31 Aircraft Pitching Motions (Journal article)
Ghoreyshi, M., Cummings, R. M., Ronch, A. D., & Badcock, K. J. (2013). Transonic Aerodynamic Load Modeling of X-31 Aircraft Pitching Motions. AIAA Journal, 51(10), 2447-2464. doi:10.2514/1.J052309DOI: 10.2514/1.J052309
2012
Accelerating convergence of the CFD Linear Frequency Domain method by a preconditioned linear solver (Conference Paper)
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).
Computational fluid dynamics framework for aerodynamic model assessment (Journal article)
Vallespin, D., Badcock, K. J., Da Ronch, A., White, M. D., Perfect, P., & Ghoreyshi, M. (2012). Computational fluid dynamics framework for aerodynamic model assessment. PROGRESS IN AEROSPACE SCIENCES, 52, 2-18. doi:10.1016/j.paerosci.2011.12.004DOI: 10.1016/j.paerosci.2011.12.004
How Structural Model Variability Influences Transonic Aeroelastic Stability (Journal article)
Marques, S., Badcock, K. J., Khodaparast, H. H., & Mottershead, J. E. (2012). How Structural Model Variability Influences Transonic Aeroelastic Stability. Journal of Aircraft, 49(5), 1189-1199. doi:10.2514/1.C031103DOI: 10.2514/1.C031103
How structural model variability influences transonic aeroelastic stability (Journal article)
Marques, S., Badcock, K. J., Khodaparast, H. H., & Mottershead, J. E. (2012). How structural model variability influences transonic aeroelastic stability. Journal of Aircraft, 49(5), 1189-1199. doi:10.2514/1.C031103DOI: 10.2514/1.C031103
Impact of structural variability on robust flflutteroptimization (Conference Paper)
Marques, S., & Badcock, K. J. (2012). Impact of structural variability on robust flflutteroptimization. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Impact of structural variability on robust flutter optimization (Conference Paper)
Marques, S., & Badcock, K. J. (2012). Impact of structural variability on robust flutter optimization. In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012.
Linear Frequency Domain and Harmonic Balance Predictions of Dynamic Derivatives (Journal article)
Da Ronch, A., McCracken, A. J., Badcock, K. J., Widhalm, M., & Campobasso, M. S. (2013). Linear Frequency Domain and Harmonic Balance Predictions of Dynamic Derivatives. Journal of Aircraft, 50(3), 694-707. doi:10.2514/1.C031674DOI: 10.2514/1.C031674
Lyapunov inverse iteration for stability analysis using computational fluid dynamics (Conference Paper)
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.
Lyapunov inverse iteration for stability analysis using computational fluid dynamics (Conference Paper)
Timme, S., Badcock, K. J., Wu, M., & Spence, A. (2012). Lyapunov inverse iteration for stability analysis using computational fluid dynamics. In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012.
Nonlinear model reduction for flexible aircraft control design (Conference Paper)
da Ronch, A., Badcock, K. J., Wang, Y., Wynn, A., & Palacios, R. (2012). Nonlinear model reduction for flexible aircraft control design. In AIAA Atmospheric Flight Mechanics Conference 2012. doi:10.2514/6.2012-4404DOI: 10.2514/6.2012-4404
Requirements for Computer Generated Aerodynamic Models for Aircraft Stability and Control Analysis (Conference Paper)
McCracken, A., Akram, U., Da Ronch, A., & Badcock, K. J. (2012). Requirements for Computer Generated Aerodynamic Models for Aircraft Stability and Control Analysis. In 5th Symposium on Integrating CFD and Experiments in Aerodynamics (pp. .). Tokyo, Japan: Integration 2012.
Semi-meshless stencil selection for anisotropic point distributions (Journal article)
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:10.1080/10618562.2012.744450DOI: 10.1080/10618562.2012.744450
Transonic Aerodynamic Loads Modeling of X-31 Aircraft (Conference Paper)
Ghoreyshi, M., Jirasek, A., Cummings, R. M., Da Ronch, A., & Badcock, K. J. (2012). Transonic Aerodynamic Loads Modeling of X-31 Aircraft. In 30th AIAA Applied Aerodynamics Conference (pp. AIAA paper 2012-3127). New Orleans, Louisiana: AIAA.
Transonic aerodynamic loads modeling of X-31 aircraft (Conference Paper)
Ghoreyshi, M., Post, M. L., Cummings, R. M., Da Ronch, A., & Badcock, K. J. (2012). Transonic aerodynamic loads modeling of X-31 aircraft. In 30th AIAA Applied Aerodynamics Conference 2012 (pp. 1824-1852).
2011
A framework for constrained control allocation using CFD-based tabular data (Conference Paper)
Da Ronch, A., Ghoreyshi, M., Vallespin, D., Badcock, K. J., Mengmeng, Z., Oppelstrup, J., & Rizzi, A. (2011). A framework for constrained control allocation using CFD-based tabular data. In 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
An implicit semi-meshless scheme with stencil selection for anisotropic point distributions (Conference Paper)
Kennett, D. J., Timme, S., Angulo, J., & Badcock, K. J. (2011). An implicit semi-meshless scheme with stencil selection for anisotropic point distributions. In 20th AIAA Computational Fluid Dynamics Conference 2011.
Analysis of conventional and asymmetric aircraft configurations using CEASIOM (Journal article)
Richardson, T. S., McFarlane, C., Isikveren, A., Badcock, K., & Da Ronch, A. (2011). Analysis of conventional and asymmetric aircraft configurations using CEASIOM. Progress in Aerospace Sciences, 47(8), 647-659. doi:10.1016/j.paerosci.2011.08.008DOI: 10.1016/j.paerosci.2011.08.008
Analysis of the Boeing 747-100 using CEASIOM (Journal article)
Richardson, T. S., Beaverstock, C., Isikveren, A., Meheri, A., Badcock, K., & Da Ronch, A. (2011). Analysis of the Boeing 747-100 using CEASIOM. Progress in Aerospace Sciences, 47(8), 660-673. doi:10.1016/j.paerosci.2011.08.009DOI: 10.1016/j.paerosci.2011.08.009
Automated CFD Analysis for the Investigation of Flight Handling Qualities (Journal article)
Ghoreyshi, M., Badcock, K. J., Da Ronch, A., Vallespin, D., & Rizzi, A. (2011). Automated CFD Analysis for the Investigation of Flight Handling Qualities. Mathematical Modelling of Natural Phenomena, 6(3), 166-188. doi:10.1051/mmnp/20116307DOI: 10.1051/mmnp/20116307
Calculating the influence of structural uncertainty on aeroelastic limit cycle response (Conference Paper)
Badcock, K. J., Khodaparast, H. H., Timme, S., & Mottershead, J. E. (2011). Calculating the influence of structural uncertainty on aeroelastic limit cycle response. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. doi:10.2514/6.2011-1741DOI: 10.2514/6.2011-1741
Evaluation of Dynamic Derivatives Using Computational Fluid Dynamics (Journal article)
Ronch, A. D., Vallespin, D., Ghoreyshi, M., & Badcock, K. J. (2012). Evaluation of Dynamic Derivatives Using Computational Fluid Dynamics. AIAA Journal, 50(2), 470-484. doi:10.2514/1.J051304DOI: 10.2514/1.J051304
Framework for Establishing Limits of Tabular Aerodynamic Models for Flight Dynamics Analysis (Journal article)
Ghoreyshi, M., Badcock, K. J., Ronch, A. D., Marques, S., Swift, A., & Ames, N. (2011). Framework for Establishing Limits of Tabular Aerodynamic Models for Flight Dynamics Analysis. Journal of Aircraft, 48(1), 42-55. doi:10.2514/1.C001003DOI: 10.2514/1.C001003
Interval Model Updating with Irreducible Uncertainty Using the Kriging Predictor (Journal article)
Khodaparast, H. H., Mottershead, J. E., & Badcock, K. J. (2011). Interval Model Updating with Irreducible Uncertainty Using the Kriging Predictor. Mechanical Systems and Signal Processing, 25, 1204-1226.
Interval model updating with irreducible uncertainty using the Kriging predictor (Journal article)
Khodaparast, H. H., Mottershead, J. E., & Badcock, K. J. (2011). Interval model updating with irreducible uncertainty using the Kriging predictor. Mechanical Systems and Signal Processing, 25(4), 1204-1226. doi:10.1016/j.ymssp.2010.10.009DOI: 10.1016/j.ymssp.2010.10.009
Modeling of unsteady aerodynamic loads (Conference Paper)
Da Ronch, A., Mccracken, A., Badcock, K. J., Ghoreyshi, M., & Cummings, R. M. (2011). Modeling of unsteady aerodynamic loads. In AIAA Atmospheric Flight Mechanics Conference 2011.
On the generation of flight dynamics aerodynamic tables by computational fluid dynamics (Journal article)
Da Ronch, A., Ghoreyshi, M., & Badcock, K. J. (2011). On the generation of flight dynamics aerodynamic tables by computational fluid dynamics. Progress in Aerospace Sciences, 47(8), 597-620. doi:10.1016/j.paerosci.2011.09.001DOI: 10.1016/j.paerosci.2011.09.001
Reducing Uncertainty in Aeroelastic Flutter Boundaries Using Experimental Data (Conference Paper)
Dwight, R. P., Bijl, H., Marques, S., & Badcock, K. J. (2011). Reducing Uncertainty in Aeroelastic Flutter Boundaries Using Experimental Data. In International Forum on Aeroelasticity and Structural Dynamics. Paris: -.
Stochastic model updating: Perturbation, interval method and Bayesian inference (Conference Paper)
Mottershead, J. E., Khodaparast, H. H., Dwight, R. P., & Badcock, K. J. (2011). Stochastic model updating: Perturbation, interval method and Bayesian inference. In Springer Proceedings in Physics Vol. 139 (pp. 13-23). doi:10.1007/978-94-007-2069-5_2DOI: 10.1007/978-94-007-2069-5_2
Transonic Aeroelastic Instability Searches Using Sampling and Aerodynamic Model Hierarchy (Journal article)
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.J050509DOI: 10.2514/1.J050509
Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation (Conference Paper)
Timme, S., Marques, S., & Badcock, K. J. (2011). Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation. In AIAA Journal Vol. 49 (pp. 1202-1213). doi:10.2514/1.J050975DOI: 10.2514/1.J050975
Transonic aeroelastic simulation for instability searches and uncertainty analysis (Journal article)
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.2011.05.002DOI: 10.1016/j.paerosci.2011.05.002
Transonic aeroelastic stability analysis using a kriging-based Schur complement formulation (Journal article)
Timme, S., Marques, S., & Badcock, K. J. (2010). Transonic aeroelastic stability analysis using a kriging-based Schur complement formulation. AIAA Atmospheric Flight Mechanics Conference 2010.
Updating Computational Aeroelastic Models using Flight Flutter Test Data (Journal article)
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.
Updating of Computational Aeroelastic Predictions using Flight Flutter Test Data (Conference Paper)
Timme, S., & Badcock, K. J. (2011). Updating of Computational Aeroelastic Predictions using Flight Flutter Test Data. In International Forum on Aeroelasticity and Structural Dynamics. Paris, France.: International Forum on Aeroelasticity and Structural Dynamics.
Validation of numerical prediction of dynamic derivatives: The DLR-F12 and the Transcruiser test cases (Journal article)
Mialon, B., Khrabrov, A., Khelil, S. B., Huebner, A., Da Ronch, A., Badcock, K., . . . Lahuta, M. (2011). Validation of numerical prediction of dynamic derivatives: The DLR-F12 and the Transcruiser test cases. Progress in Aerospace Sciences, 47(8), 674-694. doi:10.1016/j.paerosci.2011.08.010DOI: 10.1016/j.paerosci.2011.08.010
Vortical Flow Prediction Validation for an Unmanned Combat Air Vehicle Model (Journal article)
Vallespin, D., Ronch, A. D., Badcock, K. J., & Boelens, O. (2011). Vortical Flow Prediction Validation for an Unmanned Combat Air Vehicle Model. Journal of Aircraft, 48(6), 1948-1959. doi:10.2514/1.C031385DOI: 10.2514/1.C031385
2010
Adaptive aeroelastic concept applied to a civil jet aircraft model (Conference Paper)
Vio, G. A., Marques, S., Cooper, J. E., & Badcock, K. J. (2010). Adaptive aeroelastic concept applied to a civil jet aircraft model. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Applying Interpolation Techniques to Search for Transonic Aeroelastic Instability: ANN vs Kriging (Conference Paper)
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.
Assessment of the Limits of Tabular Aerodynamic Models for Flight Dynamics Analysis using the SACCON UCAV Configuration (Conference Paper)
Vallespin, D., & Badcock, K. J. (2010). Assessment of the Limits of Tabular Aerodynamic Models for Flight Dynamics Analysis using the SACCON UCAV Configuration. In RAeS Aerodynamics Conference (pp. paper). Bristol: Royal Aeronautical Society.
Bifurcation Prediction of Large-Order Aeroelastic Models (Journal article)
Badcock, K. J., & Woodgate, M. A. (2010). Bifurcation Prediction of Large-Order Aeroelastic Models. AIAA Journal, 48(6), 1037-1046. doi:10.2514/1.40961DOI: 10.2514/1.40961
Comparison of conventional and asymmetric aircraft configurations using CEASIOM (Conference Paper)
McFarlane, C., Richardson, T. S., Da Ronch, A., & Badcock, K. (2010). Comparison of conventional and asymmetric aircraft configurations using CEASIOM. In AIAA Atmospheric Flight Mechanics Conference 2010.
Computation and Evaluation of Dynamic Derivatives using CFD (Conference Paper)
Da Ronch, A., Vallespin, D., Ghoreyshi, M., & Badcock, K. J. (2010). Computation and Evaluation of Dynamic Derivatives using CFD. In 28th AIAA Applied Aerodynamics Conference (pp. AIAA Paper 2010-4817). Chicago, Illinois: AIAA.
Computation and Evaluation of Dynamic Derivatives using CFD (Conference Paper)
Da Ronch, A., Ghoreyshi, M., & Badcock, K. J. (2010). Computation and Evaluation of Dynamic Derivatives using CFD. In 28th AIAA Applied Aerodynamics Conference. Chicago: AIAA.
Computation of dynamic derivatives Using CFD (Conference Paper)
Da Ronch, A., Vallespin, D., Ghoreyshi, M., & Badcock, K. J. (2010). Computation of dynamic derivatives Using CFD. In 28th AIAA Applied Aerodynamics Conference.
Flight Manoeuvre Validation of Data Tables Generated Using an Aerodynamic Model Hierarchy (Conference Paper)
Ghoreyshi, M., Vallespin, D., Badcock, K. J., Da Ronch, A., Vos, J. B., & Hitzel, S. (2010). Flight Manoeuvre Validation of Data Tables Generated Using an Aerodynamic Model Hierarchy. In AIAA Guidance, Navigation and Control Conference (pp. AIAA Paper 2010-8239). Toronto, Canada: AIAA.
Influence of Atmospheric Variability on Transonic Aeroelasticity (Conference Paper)
Marques, S., & Badcock, K. J. (2010). Influence of Atmospheric Variability on Transonic Aeroelasticity. In Royal Aeronautical Society conference on Structural Design. London: RAeSoc.
Inter-grid transfer influence on transonic flutter predictions (Conference Paper)
Swift, A., & Badcock, K. J. (2010). Inter-grid transfer influence on transonic flutter predictions. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Interval model updating: Method and application (Conference Paper)
Khodaparast, H. H., Mottershead, J. E., & Badcock, K. J. (2010). Interval model updating: Method and application. In Proceedings of ISMA 2010 - International Conference on Noise and Vibration Engineering, including USD 2010 (pp. 5277-5289).
Linear Frequency Domain and Harmonic Balance Predictions of Dynamic Derivatives (Conference Paper)
Da Ronch, A., Badcock, K. J., Ghoreyshi, M., Gortz, S., Widhalm, M., & Dwight, R. (2010). Linear Frequency Domain and Harmonic Balance Predictions of Dynamic Derivatives. In 28th AIAA Applied Aerodynamics Conference. Chicago: AIAA.
Linear frequency domain and harmonic balance predictions of dynamic derivatives (Conference Paper)
Da Ronch, A., Ghoreyshi, M., Badcock, K. J., Görtz, S., Widhalm, M., Dwight, R. P., & Campobasso, M. S. (2010). Linear frequency domain and harmonic balance predictions of dynamic derivatives. In 28th AIAA Applied Aerodynamics Conference.
Manoeuvre Validation of Data Tables Generated Using an Aerodynamic Model Hierarchy (Conference Paper)
Ghoreyshi, M., Vallespin, D., Badcock, K. J., Da Ronch, A., Vos, J., & Hitzel, S. (2010). Manoeuvre Validation of Data Tables Generated Using an Aerodynamic Model Hierarchy. In AIAA Atmospheric Flight Mechanics Conference. Toronto: AIAA.
Propagation of structural uncertainty to linear aeroelastic stability (Journal article)
Khodaparast, H. H., Mottershead, J. E., & Badcock, K. J. (2010). Propagation of structural uncertainty to linear aeroelastic stability. Computers and Structures, 88(3-4), 223-236. doi:10.1016/j.compstruc.2009.10.005DOI: 10.1016/j.compstruc.2009.10.005
Searching for transonic aeroelastic instability using an aerodynamic model hierarchy (Conference Paper)
Timme, S., & Badcock, K. J. (2010). Searching for transonic aeroelastic instability using an aerodynamic model hierarchy. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Simulation of aircraft manoeuvres based on computational fluid dynamics (Conference Paper)
Ghoreyshit, M., Vallespin, D., Da Ronch, A., Badcock, K. J., Vos, J., & Hitzelh, S. (2010). Simulation of aircraft manoeuvres based on computational fluid dynamics. In AIAA Atmospheric Flight Mechanics Conference 2010.
Transonic Aeroelastic Stability Predictions Under the Influence of Structural Variability (Journal article)
Marques, S., Badcock, K. J., Khodaparast, H. H., & Mottershead, J. E. (2010). Transonic Aeroelastic Stability Predictions Under the Influence of Structural Variability. Journal of Aircraft, 47(4), 1229-1239. doi:10.2514/1.46971DOI: 10.2514/1.46971
Transonic aeroelastic stability predictions under the influence of structural variability (Journal article)
Marques, S., Badcock, K. J., Khodaparast, H. H., & Mottershead, J. E. (2010). Transonic aeroelastic stability predictions under the influence of structural variability. Journal of Aircraft, 47(4), 1229-1239. doi:10.2514/1.46971DOI: 10.2514/1.46971
Validation of Vortical Flow Predictions for a UCAV Wind Tunnel Model (Conference Paper)
Vallespin, D., Da Ronch, A., Boelens, O., & Badcock, K. J. (2010). Validation of Vortical Flow Predictions for a UCAV Wind Tunnel Model. In 28th AIAA Applied Aerodynamics Conference. Chicago: AIAA.
Validation of vortical flow predictions for a UCAV wind tunnel model (Conference Paper)
Vallespin, D., Da Ronch, A., Badcock, K. J., & Boelens, O. (2010). Validation of vortical flow predictions for a UCAV wind tunnel model. In 28th AIAA Applied Aerodynamics Conference.
Validation study for prediction of iced aerofoil aerodynamics (Journal article)
Marques, S., Badcock, K. J., Gooden, J. H. M., Gates, S., & Maybury, W. (2010). Validation study for prediction of iced aerofoil aerodynamics. Aeronautical Journal, 114(1152), 103-112.
2009
Accelerating the numerical generation of aerodynamic models for flight simulation (Conference Paper)
Ghoreyshi, M., Badcock, K. J., & Woodgate, M. A. (2009). Accelerating the numerical generation of aerodynamic models for flight simulation. In 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Aerodynamic modelling for flight dynamics analysis of conceptual aircraft designs (Conference Paper)
Ghoreyshi, M., Da Ronch, A., Badcock, K. J., Dees, J., Berard, A., & Rizzi K, A. (2009). Aerodynamic modelling for flight dynamics analysis of conceptual aircraft designs. In Collection of Technical Papers - AIAA Applied Aerodynamics Conference.
CFD based aeroelastic stability predictions under the influence of structural variability (Conference Paper)
Marques, S., Badcock, K. J., Khodaparast, H. H., & Mottershead, J. E. (2009). CFD based aeroelastic stability predictions under the influence of structural variability. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
European benchmark on numerical prediction of stability and control derivatives (Conference Paper)
Mialon, B., Khelil, S. B., Huebner, A., Jouhaud, J. C., Rogé, G., Hitzel, S., . . . Lahuta, M. (2009). European benchmark on numerical prediction of stability and control derivatives. In Collection of Technical Papers - AIAA Applied Aerodynamics Conference.
Framework for Establishing the Limits of Tabular Aerodynamic Models for Flight Dynamics (Conference Paper)
Ghoreyshi, M., Badcock, K. J., Da Ronch, A., Swift, A., Marques, S., & Ames, N. (2009). Framework for Establishing the Limits of Tabular Aerodynamic Models for Flight Dynamics. In AIAA Atmospheric Flight Mechanics Conference (pp. AIAA Paper 2009-6273). Chicago, Illinois: AIAA.
Generation of Aerodynamic Models for Flight Simulation (Conference Paper)
Ghoreyshi, M., Badcock, K. J., & Woodgate, M. A. (2009). Generation of Aerodynamic Models for Flight Simulation. In -. Florida: American Institute of Aeronautics and Astronautics.
Implicit Harmonic Balance Solver for Transonic Flow with Forced Motions (Journal article)
Woodgate, M. A., & Badcock, K. J. (2009). Implicit Harmonic Balance Solver for Transonic Flow with Forced Motions. AIAA Journal, 47(4), 893-901. doi:10.2514/1.36311DOI: 10.2514/1.36311
Implicit harmonic balance solver for transonic flow with forced motions (Journal article)
Woodgate, M. A., & Badcock, K. J. (2009). Implicit harmonic balance solver for transonic flow with forced motions. AIAA Journal, 47(4), 893-901. doi:10.2514/1.36311DOI: 10.2514/1.36311
Oscillatory Behavior of Transonic Aeroelastic Instability Boundaries (Journal article)
Timme, S., & Badcock, K. J. (2009). Oscillatory Behavior of Transonic Aeroelastic Instability Boundaries. AIAA Journal, 47(6), 1590-1592. doi:10.2514/1.40497DOI: 10.2514/1.40497
Shock Effects on Delta Wing Vortex Breakdown (Journal article)
Schiavetta, L. A., Boelens, O. J., Crippa, S., Cummings, R. M., Fritz, W., & Badcock, K. J. (2009). Shock Effects on Delta Wing Vortex Breakdown. Journal of Aircraft, 46(3), 903-914. doi:10.2514/1.38792DOI: 10.2514/1.38792
2007
Aeroelastic system identification using transonic CFD data for a wing/store configuration (Journal article)
Vio, G. A., Dimitriadis, G., Cooper, J. E., Badcock, K. J., Woodgate, M. A., & Rampurawala, A. M. (2007). Aeroelastic system identification using transonic CFD data for a wing/store configuration. Aerospace Science and Technology, 11(2-3), 146-154. doi:10.1016/j.ast.2006.09.003DOI: 10.1016/j.ast.2006.09.003
CFD Analysis of Rotor-Fuselage Aerodynamics based on a Sliding Mesh Algorithm (Conference Paper)
Steijl, R., Barakos, G., & Badcock, K. (2007). CFD Analysis of Rotor-Fuselage Aerodynamics based on a Sliding Mesh Algorithm. In EUCASS (pp. NA). Brussels: EUCASS Association.
Comparison of des and URANS for unsteady vortical flows over delta wings (Conference Paper)
Schiavetta, L. A., Badcock, K. J., & Cummings, R. M. (2007). Comparison of des and URANS for unsteady vortical flows over delta wings. In Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting Vol. 19 (pp. 13080-13101).
Computational Fluid Dynamics Study of Three-Dimensional Dynamic Stall of Various Planform Shapes (Journal article)
Spentzos, A., Barakos, G. N., Badcock, K. J., Richards, B. E., Coton, F. N., McD. Galbraith, R. A., . . . Favier, D. (2007). Computational Fluid Dynamics Study of Three-Dimensional Dynamic Stall of Various Planform Shapes. Journal of Aircraft, 44(4), 1118-1128. doi:10.2514/1.24331DOI: 10.2514/1.24331
Evaluation of a Simplified Grid Treatment for Oscillating Trailing-Edge Control Surfaces (Journal article)
Rampurawala, A. M., & Badcock, K. J. (2007). Evaluation of a Simplified Grid Treatment for Oscillating Trailing-Edge Control Surfaces. Journal of Aircraft, 44(4), 1177-1188. doi:10.2514/1.24623DOI: 10.2514/1.24623
Evaluation of results from a reynolds averaged multiblock code against F-16XL flight data (Conference Paper)
Badcock, K. J. (2007). Evaluation of results from a reynolds averaged multiblock code against F-16XL flight data. In Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting Vol. 9 (pp. 5896-5912).
Fast Prediction of Wing Rock Limit Cycle Oscillations Based on CFD (Conference Paper)
Badcock, K. J., Woodgate, M. A., & Beran, P. S. (2007). Fast Prediction of Wing Rock Limit Cycle Oscillations Based on CFD. In 45th Aerospace Sciences Meeting and Exhibit. Nevada: American Institute of Aeronautics and Astonautics.
Fast prediction of wing rock limit cycle oscillations based on computational fluid dynamics (Conference Paper)
Badcock, K. J., Woodgate, M. A., & Beran, P. S. (2007). Fast prediction of wing rock limit cycle oscillations based on computational fluid dynamics. In Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting Vol. 19 (pp. 12929-12939).
Flight-regime dependent Reduced Order Models of CFD/FE aeroelastic systems in transonic flow (Conference Paper)
Dimitriadis, G., Vio, G. A., Cooper, J. E., & Badcock, K. J. (2007). Flight-regime dependent Reduced Order Models of CFD/FE aeroelastic systems in transonic flow. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference Vol. 4 (pp. 3526-3539).
High performance computing and computational aerodynamics in the UK (Journal article)
Emerson, D. R., Sunderland, A. J., Ashworth, M., & Badcock, K. J. (2007). High performance computing and computational aerodynamics in the UK. The Aeronautical Journal, 111(1117), 125-131. doi:10.1017/S0001924000004383DOI: 10.1017/S0001924000004383
Numerical study of transonic cavity flows using large-eddy and detached-eddy simulation (Journal article)
Nayyar, P., Barakos, G. N., & Badcock, K. J. (2007). Numerical study of transonic cavity flows using large-eddy and detached-eddy simulation. The Aeronautical Journal, 111(1117), 153-164. doi:10.1017/S0001924000004413DOI: 10.1017/S0001924000004413
What was learned from numerical simulations of F-16XL (CAWAPI) at flight conditions (Conference Paper)
Rizzi, A., Boelens, O., Jirasek, A., & Badcock, K. (2007). What was learned from numerical simulations of F-16XL (CAWAPI) at flight conditions. In Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting Vol. 12 (pp. 8385-8420).
hock Effects on Delta Wing Vortex Breakdown (Conference Paper)
Schiavetta, L. A., Boelens, O. J., Crippa, S., Cummings, R. M., Fritz, W., & Badcock, K. J. (2007). hock Effects on Delta Wing Vortex Breakdown. In -. Reno: American Institute of Aeronautics and Astronautics.
2006
A framework for CFD analysis of helicopter rotors in hover and forward flight (Journal article)
Steijl, R., Barakos, G., & Badcock, K. (2006). A framework for CFD analysis of helicopter rotors in hover and forward flight. International Journal for Numerical Methods in Fluids, 51(8), 819-847. doi:10.1002/fld.1086DOI: 10.1002/fld.1086
A reduced damping model derived from CFD based aeroelastic simulations (Conference Paper)
Badcock, K. J., & Woodgate, M. A. (2006). A reduced damping model derived from CFD based aeroelastic simulations. In Structural Dynamics and Materials Conference. Rhode Island: American Institute of Aeronautics and Astonautics.
A reduced order model for damping derived from CFD based aeroelastic simulations (Conference Paper)
Woodgate, M. A., & Badcock, K. J. (2006). A reduced order model for damping derived from CFD based aeroelastic simulations. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference Vol. 7 (pp. 5139-5157).
Aeroelastic Damping Model Derived from Discrete Euler Equations (Journal article)
Badcock, K. J., & Woodgate, M. A. (2006). Aeroelastic Damping Model Derived from Discrete Euler Equations. AIAA Journal, 44(11), 2601-2611. doi:10.2514/1.23637DOI: 10.2514/1.23637
Aeroelastic analysis through linear and non-linear methods: a summary of flutter prediction in the PUMA DARP (Journal article)
Taylor, N. V., Allen, C. B., Gaitonde, A. L., Jones, D. P., Vio, G. A., Cooper, J. E., . . . Henshaw, M. J. D. C. (2006). Aeroelastic analysis through linear and non-linear methods: a summary of flutter prediction in the PUMA DARP. The Aeronautical Journal, 110(1107), 333-343. doi:10.1017/S0001924000013208DOI: 10.1017/S0001924000013208
Application of an implicit dual-time stepping multi-block solver to 3d unsteady flows (Chapter)
Steijl, R., Nayyar, P., Woodgate, M. A., Badcock, K. J., & Barakos, G. N. (2006). Application of an implicit dual-time stepping multi-block solver to 3d unsteady flows. In Parallel Computational Fluid Dynamics 2005 (pp. 309-316). doi:10.1016/B978-044452206-1/50037-9DOI: 10.1016/B978-044452206-1/50037-9
Modeling 3D dynamic stall using CFD and neural networks (Conference Paper)
Spentzos, A., Barakos, G. N., Badcock, K. J., & Richards, B. E. (2006). Modeling 3D dynamic stall using CFD and neural networks. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting Vol. 17 (pp. 12870-12888).
Modelling of 3D Dynamic Stall Using CFD and Neural Networks (Conference Paper)
Spentzos, A., Barakos, G. N., Badcock, K., & Richards, B. (2006). Modelling of 3D Dynamic Stall Using CFD and Neural Networks. In 44th AIAA Aerospace Sciences Meeting and Exhibit (pp. AIAA Paper 2006-1071). Reno: American Institute of Aeronautics and Astronautics.
Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks (Journal article)
Spentzos, A., Barakos, G., Badcock, K., & Richards, B. (2006). Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 220(6), 605-618. doi:10.1243/09544100JAERO101DOI: 10.1243/09544100JAERO101
Parallelisation of CFD Methods for Multi-Physics Problems (Conference Paper)
Steijl, R., Barakos, G. N., & Badcock, K. (2006). Parallelisation of CFD Methods for Multi-Physics Problems. In European Conference on Computational Fluid Dynamics (ECCOMAS CFD 2006) (pp. NA). Egmond aan Zee: European Community on Computational Methods in Applied Sciences.
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering: Guest editorial (Journal article)
Knowles, K., Saddington, A., & Badcock, K. (2006). Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering: Guest editorial. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 220(6).
Treatment of complex configurations for flutter calculations (Conference Paper)
Rampurawala, A. M., & Badcock, K. J. (2006). Treatment of complex configurations for flutter calculations. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference Vol. 8 (pp. 5818-5840).
2005
A CFD framework for analysis of helicopter rotors (Conference Paper)
Steijl, R., Barakos, G. N., & Badcock, K. J. (2005). A CFD framework for analysis of helicopter rotors. In 17th AIAA Computational Fluid Dynamics Conference.
A Framework for Accurate and Efficient CFD Analysis of Helicopter Rotors (Conference Paper)
Steijl, R., Barakos, G. N., & Badcock, K. (2005). A Framework for Accurate and Efficient CFD Analysis of Helicopter Rotors. In 1st European Conference for Aerospace Sciences (pp. NA). Moscow: EUCASS Association.
A numerical study of hypersonic turbulent film cooling (Conference Paper)
Yang, X., Badcock, K. J., Richards, B. E., & Barakos, G. N. (2005). A numerical study of hypersonic turbulent film cooling. In 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers (pp. 1891-1905).
Aeroelastic Calculations for the Hawk Aircraft Using the Euler Equations (Journal article)
Woodgate, M. A., Badcock, K. J., Rampurawala, A. M., Richards, B. E., Nardini, D., & Henshaw, M. (2005). Aeroelastic Calculations for the Hawk Aircraft Using the Euler Equations. Journal of Aircraft, 42(4), 1005-1012. doi:10.2514/1.5608DOI: 10.2514/1.5608
Aerofoil-Vortex Interaction Using the Compressible Vorticity Confinement Method (Journal article)
Morvant, R., Badcock, K. K., & Barakos, G. G. (2005). Aerofoil-Vortex Interaction Using the Compressible Vorticity Confinement Method. AIAA Journal, 43(1), 63-75. doi:10.2514/1.5177DOI: 10.2514/1.5177
Airfoil-vortex interaction using the compressible vorticity confinement method (Journal article)
Morvant, R., Badcock, K. J., Barakos, G. N., & Richards, B. E. (2005). Airfoil-vortex interaction using the compressible vorticity confinement method. AIAA Journal, 43(1), 63-75. doi:10.2514/1.5177DOI: 10.2514/1.5177
Analysis and Control of Weapon Bay Flows (Conference Paper)
Nayyar, P., Barakos, G. N., & Badcock, K. J. (2005). Analysis and Control of Weapon Bay Flows. In Flow Induced Unsteady Loads and the Impact on Military Applications (pp. NA). Budapest: NATO RTO.
Analysis and control of transonic cavity flow using DES and LES (Conference Paper)
Nayyar, P., Barakos, G. N., Badcock, K. J., & Kirkham, D. A. (2005). Analysis and control of transonic cavity flow using DES and LES. In 35th AIAA Fluid Dynamics Conference and Exhibit.
Analysis of Flapped Rotors using CFD and Indicial Methods (Conference Paper)
Gagliardi, A., Barakos, G., Beedy, J., Badcock, K., & Richards, B. (2005). Analysis of Flapped Rotors using CFD and Indicial Methods. In 61st Forum of the American Helicopter Society (pp. NA). Grapevine: American Helicopter Society.
Analysis of flapped rotors using CFD and indicial methods (Conference Paper)
Gagliardi, A., Beedy, J., Steijl, R., Barakos, G., & Badcock, K. (2005). Analysis of flapped rotors using CFD and indicial methods. In Annual Forum Proceedings - AHS International Vol. 1 (pp. 251-272).
Analysis of flapped rotors using CFD and indicial methods (Conference Paper)
Gagliardi, A., Beedy, J., Steijl, R., Barakos, G., & Badcock, K. (2005). Analysis of flapped rotors using CFD and indicial methods. In Annual Forum Proceedings - AHS International Vol. 2 (pp. 1473-1494).
Analysis of the Effect of Rotor Wake on Rotor Loading using Various Simulation Methods (Conference Paper)
Steijl, R., Barakos, G. N., & Badcock, K. J. (2005). Analysis of the Effect of Rotor Wake on Rotor Loading using Various Simulation Methods. In K. J. Bathe (Ed.), Third MIT Conference on Computational Fluid and Solid Mechanics (pp. NA). Boston: Elsevier.
Application of an Implicit Dual-time Stepping Multi-block Solver to 3D Unsteady Flows (Conference Paper)
Steijl, R., Nayyar, P., Woodgate, M. A., Badcock, K. J., & Barakos, G. N. (2005). Application of an Implicit Dual-time Stepping Multi-block Solver to 3D Unsteady Flows. In International Conference on Parallel Computational Fluid Dynamics (PCFD 2005) (pp. NA). Maryland: Elsevier.
Assessment of simulation techniques for rotor loads prediction (Conference Paper)
Steijl, R., Barakos, G., & Badcock, K. (2005). Assessment of simulation techniques for rotor loads prediction. In 3rd M.I.T. Conference on Computational Fluid and Solid Mechanics (pp. 872-875).
Buzz Simulation for a Supersonic Transport Configuration (Conference Paper)
Rampurawala, A. M., & Badcock, K. J. (2005). Buzz Simulation for a Supersonic Transport Configuration. In International Forum on Aeroelasticity and Structural Dynamics (pp. IF-005). Munich: DGLR.
CFD Study of 3D Dynamic Stall (Conference Paper)
Spentzos, A., Barakos, G., Badcock, K., & Richards, B. E. (2005). CFD Study of 3D Dynamic Stall. In 43rd AIAA Aerospace Sciences Meeting and Exhibit (pp. AIAA Paper 2005-1107). Reno: American Institute of Aeronautics and Astronautics.
CFD based simulation of Longitudinal Flight Mechanics with Control (Conference Paper)
Allan, M. R., Badcock, K. J., & Richards, B. E. (2005). CFD based simulation of Longitudinal Flight Mechanics with Control. In 43rd Aerospace Sciences Meeting (pp. NA). Nevada: AIAA-2005-0045.
CFD based simulation of longitudinal flight mechanics with control (Conference Paper)
Allan, M. R., Badcock, K. J., & Richards, B. E. (2005). CFD based simulation of longitudinal flight mechanics with control. In 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers (pp. 2121-2137).
CFD study of 3-D dynamic stall (Conference Paper)
Spentzos, A., Barakos, G., Badcock, K., & Richards, B. (2005). CFD study of 3-D dynamic stall. In 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers (pp. 381-396).
CFD study of three-dimensional dynamic stall of various planform shapes (Conference Paper)
Spentzos, A., Barakos, G. N., Badcock, K. J., & Richards, B. E. (2005). CFD study of three-dimensional dynamic stall of various planform shapes. In 30th European Rotorcraft Forum Vol. 2005 (pp. 29-54).
Development of CFD capability for full helicopter engineering analysis (Conference Paper)
Barakos, G., Steijl, R., Badcock, K., & Brocklehurst, A. (2005). Development of CFD capability for full helicopter engineering analysis. In 31st European Rotorcraft Forum Vol. 2005.
Direct Aeroelastic Bifurcation Analysis of a Symmetric Wing Based on the Euler Equations (Journal article)
Badcock, K. J., Woodgate, M. A., & Richards, B. E. (2005). Direct Aeroelastic Bifurcation Analysis of a Symmetric Wing Based on the Euler Equations. Journal of Aircraft, 42(3), 731-737. doi:10.2514/1.5323DOI: 10.2514/1.5323
Exploration of the Free Rolling Motion of a Delta Wing Configuration in a Vortical Flow (Conference Paper)
Arthur, M. T., Allan, M., Ceresola, N., Kompenhans, J., Fritz, W., Boelens, O. J., & Pranata, B. B. (2005). Exploration of the Free Rolling Motion of a Delta Wing Configuration in a Vortical Flow. In Flow Induced Unsteady Loads and the Impact on Military Applications (pp. NA). Hungary: NATO RTO.
Fast Prediction of Wing Rock Onset Based on Computational Fluid Dynamics (Conference Paper)
Badcock, K. J., Woodgate, M. A., Allan, M. R., & Beran, P. S. (2005). Fast Prediction of Wing Rock Onset Based on Computational Fluid Dynamics. In International Forum on Aeroelasticity and Structural Dynamics (pp. IF). Munich: DGLR.
Investigation of Three-Dimensional Dynamic Stall Using Computational Fluid Dynamics (Journal article)
Spentzos, A., Barakos, G. N., Badcock, K. J., Richards, B. E., Wernert, P., Schreck, S., & Raffel, M. (2005). Investigation of Three-Dimensional Dynamic Stall Using Computational Fluid Dynamics. AIAA Journal, 43(5), 1023-1033. doi:10.2514/1.8830DOI: 10.2514/1.8830
Noise Suppression Methods for Transonic Cavity Flows (Conference Paper)
Nayyar, P., Barakos, G., Badcock, K., & Richards, B. E. (2005). Noise Suppression Methods for Transonic Cavity Flows. In CEAS/KATnet Conference on Key Aerodynamic Technologies, Bremen, Germany (pp. NA). Bremen: DGLR.
Numerical Study of Film Cooling in Hypersonic Turbulent Flow' (Conference Paper)
Yang, X., Badcock, K., Richards, B. E., & Barakos, G. N. (2005). Numerical Study of Film Cooling in Hypersonic Turbulent Flow'. In 43rd AIAA Aerospace Sciences Meeting and Exhibit (pp. AIAA Paper 2005-386). Reno: American Institute of Aeronautics and Astronautics.
Numerical investigation of 3D Dynamic Stall in rotation using CFD and neural networks (Conference Paper)
Spentzos, A., Barakos, G., & Badcock, K. (2005). Numerical investigation of 3D Dynamic Stall in rotation using CFD and neural networks. In 31st European Rotorcraft Forum Vol. 2005.
Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics (Journal article)
Gursul, I., Allan, M. R., & Badcock, K. J. (2005). Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics. Aerospace Science and Technology, 9(3), 181-189. doi:10.1016/j.ast.2004.08.007DOI: 10.1016/j.ast.2004.08.007
Towards an aero-servo-elastic simulation capability for high performance fighter aircraft (Conference Paper)
Boelens, O. J., Prananta, B. B., Soemartwoto, B. I., Allan, M. R., Badcock, K. J., & Fritz, W. (2005). Towards an aero-servo-elastic simulation capability for high performance fighter aircraft. In Flow Induced Unsteady Loads and the Impact on Military Applications (pp. NA). Hungary: NATO RTO.
Treatment of Forced Flap Motions for Aeroelastic Simulations of an Arrow Wing (Conference Paper)
Rampurawala, A. M., & Badcock, K. J. (2005). Treatment of Forced Flap Motions for Aeroelastic Simulations of an Arrow Wing. In AIAA Applied Aerodynamics Conference (pp. NA). Toronto: AIAA-2005-4962.
Treatment of forced flap motions for aeroelastic simulations of an arrow wing (Conference Paper)
Rampurawala, A. M., & Badcock, K. J. (2005). Treatment of forced flap motions for aeroelastic simulations of an arrow wing. In Collection of Technical Papers - AIAA Applied Aerodynamics Conference Vol. 2 (pp. 719-734).
Wind-Tunnel Interference Effects on Delta Wing Aerodynamics Computational Fluid Dynamics Investigation (Journal article)
Allan, M. R., Badcock, K. J., Barakos, G. N., & Richards, B. E. (2005). Wind-Tunnel Interference Effects on Delta Wing Aerodynamics Computational Fluid Dynamics Investigation. Journal of Aircraft, 42(1), 189-198. doi:10.2514/1.5324DOI: 10.2514/1.5324
2003
A RANS investigation of wind tunnel interference effects on delta wing aerodynamics (Conference Paper)
Allan, M. R., Badcock, K. J., Barakos, G. N., & Richards, B. E. (2003). A RANS investigation of wind tunnel interference effects on delta wing aerodynamics. In 21st AIAA Applied Aerodynamics Conference.
A numerical study of hypersonic laminar film cooling (Journal article)
Yang, X., Badcock, K. J., & Richards, B. E. (2003). A numerical study of hypersonic laminar film cooling. Aeronautical Journal, 107(1074), 479-486.
Extrapolation Effects on Coupled Computational Fluid Dynamics/Computational Structural Dynamics Simulations (Journal article)
L. Goura, G. S., Badcock, K. J., Woodgate, M. A., & Richards, B. E. (2003). Extrapolation Effects on Coupled Computational Fluid Dynamics/Computational Structural Dynamics Simulations. AIAA Journal, 41(2), 312-314. doi:10.2514/2.1946DOI: 10.2514/2.1946
Extrapolation effects on coupled CFD-CSD simulations (Journal article)
Goura, G. S. L., Badcock, K. J., Woodgate, M., & Richards, B. E. (2003). Extrapolation effects on coupled CFD-CSD simulations. AIAA Journal, 41(2), 312-314. Retrieved from http://www.aiaa.org/content.cfm?pageid=318
Non-linear analysis of stall flutter based on the ONERA aerodynamic model (Journal article)
Beedy, J., Barakos, G., Badcock, K. J., & Richards, B. E. (2003). Non-linear analysis of stall flutter based on the ONERA aerodynamic model. Aeronautical Journal, 107(1074), 495-509.
Numerical simulation of film cooling in hypersonic flows (Conference Paper)
Yang, X., Badcock, K. J., Richards, B. E., & Barakos, G. N. (2003). Numerical simulation of film cooling in hypersonic flows. In 36th AIAA Thermophysics Conference.
Surge wave propagation modelling using computational fluid dynamics (Conference Paper)
Menzies, R. D. D., Badcock, K. J., Barakos, G. N., & Richards, B. E. (2003). Surge wave propagation modelling using computational fluid dynamics. In 21st AIAA Applied Aerodynamics Conference.
2002
A CFD investigation of wind tunnel wall influences on pitching delta wings (Conference Paper)
Allans, M. R., Badcock, K. J., & Richards, B. E. (2002). A CFD investigation of wind tunnel wall influences on pitching delta wings. In 20th AIAA Applied Aerodynamics Conference.
A computational investigation of 3-D flow effects on micronozzles (Journal article)
Menzies, R. D. D., Richards, B. E., Badcock, K. J., Loeseken, J. L., & Kahl, M. A. (2002). A computational investigation of 3-D flow effects on micronozzles. Journal of Spacecraft and Rockets, 34(4).
Computational investigation of three-dimensional flow effects on micronozzles (Journal article)
Menzies, R. D. D., Richards, B. E., Badcock, K. J., Löseken, J., & Kahl, M. (2002). Computational investigation of three-dimensional flow effects on micronozzles. Journal of Spacecraft and Rockets, 39(4), 642.
Utilising CFD in the investigation of high-speed unsteady spiked body flows (Journal article)
Feszty, D., Badcock, K. J., & Richards, B. E. (2002). Utilising CFD in the investigation of high-speed unsteady spiked body flows. Aeronautical Journal, 106(1058), 161-174.
Validation of the simulation of flow in an S-Duct (Conference Paper)
Menzies, R. D. D., Badcock, K. J., Barakos, G. N., & Richards, B. E. (2002). Validation of the simulation of flow in an S-Duct. In 20th AIAA Applied Aerodynamics Conference.
2000
A grid deformation technique for unsteady flow computations (Journal article)
Dubuc, L., Cantariti, F., Woodgate, M., Gribben, B., Badcock, K. J., & Richards, B. E. (2000). A grid deformation technique for unsteady flow computations. International Journal for Numerical Methods in Fluids, 32(3), 285-311. doi:3.0.CO;2-C">10.1002/(SICI)1097-0363(20000215)32:3<285::AID-FLD939>3.0.CO;2-CDOI: 10.1002/(SICI)1097-0363(20000215)32:3<285::AID-FLD939>3.0.CO;2-C
Accelerating the Numerical Generation of Aerodynamic Models for Flight Simulation (Journal article)
Ghoreyshi, M., Badcock, K. J., & Woodgate, M. A. (2009). Accelerating the Numerical Generation of Aerodynamic Models for Flight Simulation. Journal of Aircraft, 46(3), 972-980. doi:10.2514/1.39626DOI: 10.2514/1.39626
Comparison of Measured and Block Structured Simulation Results for the F-16XL Aircraft (Journal article)
Boelens, O. J., Badcock, K. J., Elmilgui, A., Abdol-Hamid, K. S., & Massey, S. J. (2009). Comparison of Measured and Block Structured Simulation Results for the F-16XL Aircraft. Journal of Aircraft, 46(2), 377-384. doi:10.2514/1.35064DOI: 10.2514/1.35064
EROS — a common European Euler code for the analysis of the helicopter rotor flowfield (Journal article)
Renzoni, P., D'Alascio, A., Kroll, N., Peshkin, D., Hounjet, M. H. L., Boniface, J. -C., . . . Kokkalis, A. (2000). EROS — a common European Euler code for the analysis of the helicopter rotor flowfield. Progress in Aerospace Sciences, 36(5-6), 437-485. doi:10.1016/S0376-0421(00)00006-3DOI: 10.1016/S0376-0421(00)00006-3
Elements of computational fluid dynamics on block structured grids using implicit solvers (Journal article)
Badcock, K. J., Richards, B. E., & Woodgate, M. A. (2000). Elements of computational fluid dynamics on block structured grids using implicit solvers. Progress in Aerospace Sciences, 36(5-6), 351-392. doi:10.1016/S0376-0421(00)00005-1DOI: 10.1016/S0376-0421(00)00005-1
F16-XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project International (Journal article)
Boelens, O. J., Badcock, K. J., Görtz, S., Morton, S., Fritz, W., Karman, S. L., . . . Lamar, J. E. (2009). F16-XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project International. Journal of Aircraft, 46(2), 369-376. doi:10.2514/1.34852DOI: 10.2514/1.34852
International Journal for Numerical Methods in Fluids (Journal article)
Dubuc, L., Cantariti, F., Woodgate, M., Gribben, B. J., Badcock, K. J., & Richards, B. E. (2000). International Journal for Numerical Methods in Fluids. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 32(3), 285-311.
Lessons Learned from Numerical Simulations of the F-16XL Aircraft at Flight Conditions (Journal article)
Rizzi, A., Jirásek, A., Lamar, J. E., Crippa, S., Badcock, K. J., & Boelens, O. J. (2009). Lessons Learned from Numerical Simulations of the F-16XL Aircraft at Flight Conditions. Journal of Aircraft, 46(2), 423-441. doi:10.2514/1.35698DOI: 10.2514/1.35698
Non-linear aeroelastic prediction for aircraft applications (Journal article)
Henshaw, M. J. D. C., Badcock, K. J., Vio, G. A., Allen, C. B., Chamberlain, J., Kaynes, I., . . . Denley, C. J. (2007). Non-linear aeroelastic prediction for aircraft applications. PROGRESS IN AEROSPACE SCIENCES, 43(4-6), 65-137. doi:10.1016/j.paerosci.2007.05.002DOI: 10.1016/j.paerosci.2007.05.002
Numerical simulation of a pulsating flow arising over an axisymmetric spiked blunt body at Mach 2.21 and Mach 6.00 (Journal article)
Feszty, D., Richards, B. E., Badcock, K. J., & Woodgate, M. A. (2000). Numerical simulation of a pulsating flow arising over an axisymmetric spiked blunt body at Mach 2.21 and Mach 6.00. Shock Waves, 10(5), 321-323.
Numerical simulation of a pulsating flow arising over an axisymmetric spiked blunt body at Mach 2.21 and Mach 6.00 (Journal article)
Feszty, D., Richards, B. E., Badcock, K. J., & Woodgate, M. A. (2000). Numerical simulation of a pulsating flow arising over an axisymmetric spiked blunt body at Mach 2.21 and Mach 6.00. Shock Waves, 10(5), 323-331. doi:10.1007/s001930000065DOI: 10.1007/s001930000065
Numerical simulation of the hysteresis phenomenon in high-speed spiked body flows (Conference Paper)
Feszty, D., Badcock, K. J., & Richards, B. E. (2000). Numerical simulation of the hysteresis phenomenon in high-speed spiked body flows. In 38th Aerospace Sciences Meeting and Exhibit.
Numerical study of shock-reflection hysteresis in an underexpanded jet (Journal article)
Gribben, B. J., Badcock, K. J., & Richards, B. E. (2000). Numerical study of shock-reflection hysteresis in an underexpanded jet. AIAA journal, 38(2), 275-283. doi:10.2514/2.954DOI: 10.2514/2.954
Simulation of unsteady turbulent flows around moving aerofoils using the pseudo-time method (Journal article)
Badcock, K. J., Cantariti, F., Hawkins, I., Woodgate, M., Dubuc, L., & Richards, B. E. (2000). Simulation of unsteady turbulent flows around moving aerofoils using the pseudo-time method. International Journal for Numerical Methods in Fluids, 32(5), 585-604. doi:3.0.CO;2-1">10.1002/(SICI)1097-0363(20000315)32:5<585::AID-FLD976>3.0.CO;2-1DOI: 10.1002/(SICI)1097-0363(20000315)32:5<585::AID-FLD976>3.0.CO;2-1
Solution of the unsteady Euler equations in three dimensions using a fully unfactored method (Conference Paper)
Badcock, K., Woodgate, M., Cantariti, F., & Richards, B. (2000). Solution of the unsteady Euler equations in three dimensions using a fully unfactored method. In 38th Aerospace Sciences Meeting and Exhibit.
Subsonic and transonic transitional cavity flows (Conference Paper)
Henderson, J., Badcock, K., & Richards, B. E. (2000). Subsonic and transonic transitional cavity flows. In 6th Aeroacoustics Conference and Exhibit.
Time accurate euler calculations of vortical flow on a delta wing in rolling motion (Conference Paper)
Woodgate, M., Badcock, K., & Richards, B. (2000). Time accurate euler calculations of vortical flow on a delta wing in rolling motion. In European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2000.
Understanding subsonic and transonic open cavity flows and supression of cavity tones (Conference Paper)
Henderson, J., Badcock, K., & Richards, B. (2000). Understanding subsonic and transonic open cavity flows and supression of cavity tones. In 38th Aerospace Sciences Meeting and Exhibit.
Wing-Rock Limit Cycle Oscillation Prediction Based on Computational Fluid Dynamics (Journal article)
Badcock, K. J., Woodgate, M. A., Allan, M. R., & Beran, P. S. (2008). Wing-Rock Limit Cycle Oscillation Prediction Based on Computational Fluid Dynamics. Journal of Aircraft, 45(3), 954-961. doi:10.2514/1.32812DOI: 10.2514/1.32812