IOP conference series: earth and environmental science J Huang, G Zeng, X Li, X Cheng, H Tong IOP publishing, 1995 | 784* | 1995 |
A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization S Nadarajah, A Jameson 38th Aerospace sciences meeting and exhibit, 667, 2000 | 456 | 2000 |
Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization S Nadarajah, A Jameson 15th AIAA computational fluid dynamics conference, 2530, 2001 | 171 | 2001 |
Optimum shape design for unsteady flows with time-accurate continuous and discrete adjoint method SK Nadarajah, A Jameson AIAA journal 45 (7), 1478-1491, 2007 | 134 | 2007 |
Effect of shape parameterization on aerodynamic shape optimization P Castonguay, S Nadarajah 45th AIAA Aerospace Sciences Meeting and Exhibit, 59, 2007 | 130 | 2007 |
Survey of shape parameterization techniques and its effect on three-dimensional aerodynamic shape optimization S Nadarajah, P Castonguay, A Mousavi 18th AIAA computational fluid dynamics conference, 3837, 2007 | 109 | 2007 |
The discrete adjoint approach to aerodynamic shape optimization SK Nadarajah stanford university, 2003 | 105 | 2003 |
Optimum shape design for unsteady three-dimensional viscous flows using a nonlinear frequency-domain method SK Nadarajah, A Jameson Journal of Aircraft 44 (5), 1513-1527, 2007 | 94 | 2007 |
Optimal control of unsteady flows using time accurate and non-linear frequency domain methods S Nadarajah, M McMullen, A Jameson 33rd AIAA Fluid Dynamics Conference and Exhibit, 3875, 2003 | 90 | 2003 |
Implicit large eddy simulation using the high‐order correction procedure via reconstruction scheme BC Vermeire, S Nadarajah, PG Tucker International Journal for Numerical Methods in Fluids 82 (5), 231-260, 2016 | 80 | 2016 |
Constrained adjoint-based aerodynamic shape optimization of a single-stage transonic compressor B Walther, S Nadarajah Journal of turbomachinery 135 (2), 021017, 2013 | 78 | 2013 |
Toward real-time aero-icing simulation of complete aircraft via FENSAP-ICE K Nakakita, S Nadarajah, W Habashi Journal of Aircraft 47 (1), 96-109, 2010 | 72 | 2010 |
Adjoint-based aerodynamic optimization of benchmark problems S Nadarajah 53rd AIAA aerospace sciences meeting, 1948, 2015 | 63 | 2015 |
Sonic boom reduction using an adjoint method for wing-body configurations in supersonic flow S Nadarajah, A Jameson, J Alonso 9th AIAA/ISSMO symposium on multidisciplinary analysis and optimization, 5547, 2002 | 63 | 2002 |
An adjoint method for the calculation of remote sensitivities in supersonic flow SK Nadarajah, A Jameson, J Alonso International Journal of Computational Fluid Dynamics 20 (2), 61-74, 2006 | 44 | 2006 |
Equivalence between the energy stable flux reconstruction and filtered discontinuous Galerkin schemes P Zwanenburg, S Nadarajah Journal of Computational Physics 306, 343-369, 2016 | 41 | 2016 |
Adjoint-based constrained aerodynamic shape optimization for multistage turbomachines B Walther, S Nadarajah Journal of Propulsion and Power 31 (5), 1298-1319, 2015 | 41 | 2015 |
Optimum shape design for multirow turbomachinery configurations using a discrete adjoint approach and an efficient radial basis function deformation scheme for complex … B Walther, S Nadarajah Journal of Turbomachinery 137 (8), 081006, 2015 | 41 | 2015 |
Laminar‐turbulent flow simulation for wind turbine profiles using the γ– transition model P Khayatzadeh, S Nadarajah Wind Energy 17 (6), 901-918, 2014 | 40 | 2014 |
Implicit multigrid schemes for challenging aerodynamic simulations on block-structured grids JS Cagnone, K Sermeus, SK Nadarajah, E Laurendeau Computers & fluids 44 (1), 314-327, 2011 | 31 | 2011 |