| Year |
Citation |
Score |
| 2020 |
Yang L, Jiang Y, Nadarajah S. An Extended Eddy-Preserving Scheme for Strong Vortical Flows Journal of Fluids Engineering-Transactions of the Asme. 142. DOI: 10.1115/1.4045982 |
0.442 |
|
| 2020 |
Navah F, Nadarajah S. On the verification of CFD solvers of all orders of accuracy on curved wall-bounded domains and for realistic RANS flows Computers & Fluids. 205: 104504. DOI: 10.1016/J.Compfluid.2020.104504 |
0.52 |
|
| 2020 |
Kashi A, Vangara S, Nadarajah S, Castonguay P. Asynchronous fine-grain parallel implicit smoother in multigrid solvers for compressible flow Computers & Fluids. 198: 104255. DOI: 10.1016/J.Compfluid.2019.104255 |
0.452 |
|
| 2020 |
Quaegebeur S, Nadarajah S. Insights on the coercivity of the ESFR methods for elliptic problems Computers & Mathematics With Applications. 80: 2029-2044. DOI: 10.1016/J.Camwa.2020.09.001 |
0.416 |
|
| 2019 |
Brown DA, Nadarajah S, Yang H, Castonguay P, Raiesi H, Sermeus K, Germain P. Quality-Preserving Linear Elasticity Mesh Movement Algorithm for Multi-Element Unstructured Meshes Aiaa Journal. 57: 521-531. DOI: 10.2514/1.J057463 |
0.32 |
|
| 2019 |
Chen C, Nadarajah S. GCRO with dynamic deflated restarting for solving adjoint systems of equations for aerodynamic shape optimization International Journal of Numerical Methods For Heat & Fluid Flow. 29: 2179-2205. DOI: 10.1108/Hff-10-2018-0586 |
0.406 |
|
| 2019 |
Quaegebeur S, Nadarajah S. Stability of energy stable flux reconstruction for the diffusion problem using the interior penalty and Bassi and Rebay II numerical fluxes for linear triangular elements Journal of Computational Physics. 380: 88-118. DOI: 10.1016/J.Jcp.2018.12.017 |
0.445 |
|
| 2019 |
Chen C, Nadarajah S, Castonguay P. A dynamically deflated GMRES adjoint solver for aerodynamic shape optimization Computers & Fluids. 179: 490-507. DOI: 10.1016/J.Compfluid.2018.11.016 |
0.579 |
|
| 2019 |
Benoit M, Nadarajah S. On the Geometric Conservation Law for the Non Linear Frequency Domain and Time-Spectral methods Computer Methods in Applied Mechanics and Engineering. 355: 690-728. DOI: 10.1016/J.Cma.2019.04.002 |
0.537 |
|
| 2018 |
Desterac D, Carrier G, Anderson G, Nadarajah S, Poole D, Vassberg J, Zingg D. An Example of a Pitfall in Aerodynamic Shape Optimization Aiaa Journal. 56: 1532-1540. DOI: 10.2514/1.J056128 |
0.435 |
|
| 2018 |
Najafiyazdi M, Mongeau L, Nadarajah S. Low-dissipation low-dispersion explicit Taylor-Galerkin schemes from the Runge-Kutta kernels International Journal of Aeroacoustics. 17: 88-113. DOI: 10.1177/1475472X17743657 |
0.313 |
|
| 2018 |
Shi-Dong D, Nadarajah S. Approximate Hessian for accelerated convergence of aerodynamic shape optimization problems in an adjoint-based framework Computers & Fluids. 168: 265-284. DOI: 10.1016/J.Compfluid.2018.04.019 |
0.523 |
|
| 2018 |
Navah F, Nadarajah S. A comprehensive high-order solver verification methodology for free fluid flows Aerospace Science and Technology. 80: 101-126. DOI: 10.1016/J.Ast.2018.07.006 |
0.459 |
|
| 2018 |
Brown DA, Nadarajah S. Inexactly constrained discrete adjoint approach for steepest descent-based optimization algorithms Numerical Algorithms. 78: 983-1000. DOI: 10.1007/S11075-017-0409-7 |
0.466 |
|
| 2017 |
Tardif P, Nadarajah S. Three-Dimensional Aeroelastic Solutions via the Nonlinear Frequency-Domain Method Aiaa Journal. 55: 3553-3569. DOI: 10.2514/1.J054849 |
0.576 |
|
| 2016 |
Poirier V, Nadarajah S. Efficient Reduced-Radial Basis Function-Based Mesh Deformation Within an Adjoint-Based Aerodynamic Optimization Framework Journal of Aircraft. 53: 1905-1921. DOI: 10.2514/1.C033573 |
0.434 |
|
| 2016 |
Zwanenburg P, Nadarajah S. Equivalence between the Energy Stable Flux Reconstruction and Filtered Discontinuous Galerkin Schemes Journal of Computational Physics. 306: 343-369. DOI: 10.1016/J.Jcp.2015.11.036 |
0.355 |
|
| 2016 |
Vermeire BC, Nadarajah S, Tucker PG. Implicit large eddy simulation using the high-order correction procedure via reconstruction scheme International Journal For Numerical Methods in Fluids. DOI: 10.1002/Fld.4214 |
0.432 |
|
| 2015 |
Tardif PO, Nadarajah SK. Dynamic mesh deformation with radial basis functions for the non-linear frequency domain method 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-1260 |
0.478 |
|
| 2015 |
Walther B, Nadarajah S. Adjoint-Based Constrained Aerodynamic Shape Optimization for Multistage Turbomachines Journal of Propulsion and Power. 31: 1298-1319. DOI: 10.2514/1.B35433 |
0.58 |
|
| 2015 |
Walther B, Nadarajah S. Optimum Shape Design for Multirow Turbomachinery Configurations Using a Discrete Adjoint Approach and an Efficient Radial Basis Function Deformation Scheme for Complex Multiblock Grids Journal of Turbomachinery-Transactions of the Asme. 137: 81006. DOI: 10.1115/1.4029550 |
0.593 |
|
| 2015 |
Vermeire BC, Nadarajah S. Adaptive IMEX schemes for high-order unstructured methods Journal of Computational Physics. 280: 261-286. DOI: 10.1016/J.Jcp.2014.09.016 |
0.495 |
|
| 2014 |
Khayatzadeh P, Nadarajah S. Laminar‐turbulent flow simulation for wind turbine profiles using the γ–Re˜θt transition model Wind Energy. 17: 901-918. DOI: 10.1002/We.1606 |
0.397 |
|
| 2013 |
Borna A, Habashi WG, McClure G, Nadarajah SK. CFD-FSI simulation of vortex-induced vibrations of a circular cylinder with low mass-damping Wind and Structures, An International Journal. 16: 411-431. DOI: 10.12989/Was.2013.16.5.411 |
0.471 |
|
| 2013 |
Walther B, Nadarajah S. Constrained Adjoint-Based Aerodynamic Shape Optimization of a Single-Stage Transonic Compressor Journal of Turbomachinery-Transactions of the Asme. 135: 21017. DOI: 10.1115/1.4007502 |
0.334 |
|
| 2013 |
Mosahebi A, Nadarajah S. An adaptive Non-Linear Frequency Domain method for viscous flows Computers & Fluids. 75: 140-154. DOI: 10.1016/J.Compfluid.2012.12.016 |
0.529 |
|
| 2013 |
Cagnone JS, Vermeire BC, Nadarajah SK. A polynomial adaptive LCP scheme for viscous compressible flows 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.41 |
|
| 2013 |
Mosahebi A, Nadarajah SK. Algorithmic advanced for the adaptive Non-Linear Frequency Domain Method 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.531 |
|
| 2012 |
Mohamed K, Nadarajah S, Paraschivoiu M. Eddy-Preserving Limiter for Unsteady Subsonic Flows Aiaa Journal. 50: 429-446. DOI: 10.2514/1.J051200 |
0.469 |
|
| 2012 |
Cagnone JS, Nadarajah SK. A stable interface element scheme for the p-adaptive lifting collocation penalty formulation Journal of Computational Physics. 231: 1615-1634. DOI: 10.1016/J.Jcp.2011.10.018 |
0.414 |
|
| 2012 |
Khayatzadeh P, Nadarajah SK. Aerodynamic shape optimization of natural laminar flow (NLF) airfoils 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.402 |
|
| 2011 |
Cagnone JS, Sermeus K, Nadarajah SK, Laurendeau E. Implicit multigrid schemes for challenging aerodynamic simulations on block-structured grids Computers and Fluids. 44: 314-327. DOI: 10.1016/J.Compfluid.2011.01.014 |
0.425 |
|
| 2010 |
Mousavi A, Nadarajah SK. Heat transfer optimization of gas turbine blades using an adjoint approach 13th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference 2010. DOI: 10.2514/6.2010-9048 |
0.426 |
|
| 2010 |
Nakakita K, Nadarajah S, Habashi W. Toward Real-Time Aero-Icing Simulation of Complete Aircraft via FENSAP-ICE Journal of Aircraft. 47: 96-109. DOI: 10.2514/1.44077 |
0.328 |
|
| 2010 |
Nadarajah SK, Tatossian C. Multi-objective aerodynamic shape optimization for unsteady viscous flows Optimization and Engineering. 11: 67-106. DOI: 10.1007/S11081-008-9036-4 |
0.594 |
|
| 2010 |
Mousavi A, Nadarajah SK. An adjoint-based shape optimization of gas turbine blades 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.442 |
|
| 2010 |
Mosahebi A, Nadarajah SK. An adaptive non-linear frequency domain method for viscous periodic steady state flows 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.523 |
|
| 2009 |
Mohamed K, Nadarajah S, Paraschivoiu M. Detached-Eddy Simulation of a Wing Tip Vortex at Dynamic Stall Conditions Journal of Aircraft. 46: 1302-1313. DOI: 10.2514/1.40685 |
0.36 |
|
| 2009 |
Cagnone JS, Nadarajah SK. Implicit nonlinear frequency-domain spectral-difference scheme for periodic euler flow Aiaa Journal. 47: 361-372. DOI: 10.2514/1.37978 |
0.583 |
|
| 2009 |
Cagnone JS, Nadarajah SK. A NLFD-spectral difference scheme for periodic transonic inviscid flows 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.51 |
|
| 2009 |
Cagnone JS, Nadarajah SK. A NLFD-spectral difference scheme for unsteady flows Computational Fluid Dynamics 2008. 397-402. |
0.336 |
|
| 2009 |
Soucy O, Nadarajah SK. A NLFD method for the simulation of periodic unsteady flows for overset meshes 19th Aiaa Computational Fluid Dynamics Conference. |
0.515 |
|
| 2008 |
Kachra F, Nadarajah SK. Aeroelastic solutions using the nonlinear frequency-domain method Aiaa Journal. 46: 2202-2210. DOI: 10.2514/1.27602 |
0.543 |
|
| 2008 |
Tatossian CA, Nadarajah SK, Castonguay P. Aerodynamic shape optimization of hovering rotor blades using a non-linear frequency domain approach 46th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.1016/J.Compfluid.2011.06.014 |
0.515 |
|
| 2008 |
Nadarajah SK, Tatossian CA. Adjoint-based aerodynamic shape optimization of rotorcraft blades Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. |
0.476 |
|
| 2007 |
Nadarajah SK, Jameson A. Optimum shape design for unsteady three-dimensional viscous flows using a nonlinear frequency-domain method Journal of Aircraft. 44: 1513-1527. DOI: 10.2514/1.27601 |
0.743 |
|
| 2007 |
Nadarajah SK, Jameson A. Optimum shape design for unsteady flows with time-accurate continuous and discrete adjoint methods Aiaa Journal. 45: 1478-1491. DOI: 10.2514/1.24332 |
0.721 |
|
| 2007 |
Nadarajah SK. Convergence studies of the time accurate and non-linear frequency domain methods for optimum shape design International Journal of Computational Fluid Dynamics. 21: 189-207. DOI: 10.1080/10618560701577328 |
0.605 |
|
| 2007 |
Castonguay P, Nadarajah SK. Effect of shape parameterization on aerodynamic shape optimization Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 1: 561-580. |
0.394 |
|
| 2007 |
Tatossian C, Nadarajah SK. Multi-objective constrained optimization using a non-linear frequency domain based adjoint approach Annual Forum Proceedings - Ahs International. 1: 652-662. |
0.498 |
|
| 2007 |
Mousavi A, Castonguay P, Nadarajah SK. Survey of shape parameterization techniques and its effect on three-dimensional aerodynamic shape optimization Collection of Technical Papers - 18th Aiaa Computational Fluid Dynamics Conference. 1: 234-254. |
0.385 |
|
| 2007 |
Nadarajah SK, Soucy O, Balloch C. Sonic boom reduction via remote inverse adjoint approach Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 1: 513-530. |
0.522 |
|
| 2007 |
Tatossian CA, Nadarajah SK. Time-varying objective functions for optimum shape design via control theory Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 22: 15227-15243. |
0.47 |
|
| 2007 |
Tatossian CA, Nadarajah SK. Optimum shape design of helicopter rotors in forward flight via control theory Collection of Technical Papers - 18th Aiaa Computational Fluid Dynamics Conference. 1: 436-453. |
0.442 |
|
| 2006 |
Nadarajah SK, McMullen MS, Jameson A. Aerodynamic shape optimization for unsteady three-dimensional flows International Journal of Computational Fluid Dynamics. 20: 533-548. DOI: 10.1080/10618560601088343 |
0.759 |
|
| 2006 |
Kachra F, Nadarajah SK. Aeroelastic solutions using the time accurate and non-linear frequency domain methods Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 7: 5207-5219. |
0.481 |
|
| 2006 |
Nadarajah SK, Jameson A. Optimum shape design for unsteady three- dimensional viscous flows using a non- linear frequency domain method Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. 3: 1401-1422. |
0.657 |
|
| 2006 |
Kachra F, Nadarajah SK. Viscous aeroelastic solutions using the non-linear frequency domain method Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. 1: 362-376. |
0.5 |
|
| 2006 |
Nadarajah SK, McMullen MS, Jameson A. Non-linear frequency domain based optimum shape design for unsteady three-dimensional flows Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 17: 12627-12644. |
0.768 |
|
| 2005 |
Nadarajah SK, Jameson A, Alonso J. Adjoint-Based Sonic Boom Reduction for Wing-Body Configurations in Supersonic Flow Canadian Aeronautics and Space Journal. 51: 187-199. DOI: 10.5589/Q05-014 |
0.694 |
|
| 2005 |
Nadarajah SK, Jameson A, Alonso J. Adjoint-based sonic boom reduction for wing-body configurations in supersonic flow Canadian Aeronautics and Space Journal. 51: 187-199. |
0.545 |
|
| 2003 |
Nadarajah SK, Kim S, Jameson A, Alonso JJ. Sonic boom reduction using an adjoint method for supersonic transport aircraft configurations Fluid Mechanics and Its Applications. 73: 355-362. DOI: 10.1007/978-94-010-0017-8_53 |
0.521 |
|
| 2003 |
Nadarajah SK, McMullen MS, Jameson A. Optimum shape design for unsteady flows using time accurate and non-linear frequency domain methods 33rd Aiaa Fluid Dynamics Conference and Exhibit. |
0.76 |
|
| 2002 |
Nadarajah SK, Jameson A, Alonso J. An adjoint method for the calculation of remote sensitivities in supersonic flow 40th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.1080/10618560600638114 |
0.695 |
|
| 2002 |
Nadarajah SK, Jameson A. Optimal control of unsteady flows using a time accurate method 9th Aiaa/Issmo Symposium On Multidisciplinary Analysis and Optimization. |
0.572 |
|
| 2002 |
Nadarajah SK, Jameson A, Alonso JJ. Sonic boom reduction using an adjoint method for wing-body configurations in supersonic flow 9th Aiaa/Issmo Symposium On Multidisciplinary Analysis and Optimization. |
0.56 |
|
| 2001 |
Nadarajah SK, Jameson A. Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization 15th Aiaa Computational Fluid Dynamics Conference. |
0.468 |
|
| 2000 |
Nadarajah SK, Jameson A. A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization 38th Aerospace Sciences Meeting and Exhibit. |
0.454 |
|
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