Siva Nadarajah
Title
Cited by
Cited by
Year
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
3312000
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
1392001
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
952007
Effect of shape parameterization on aerodynamic shape optimization
P Castonguay, S Nadarajah
45th AIAA Aerospace Sciences Meeting and Exhibit, 59, 2007
922007
The discrete adjoint approach to aerodynamic shape optimization
SK Nadarajah
stanford university, 2003
862003
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
852007
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
782007
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
752003
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
522002
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
512010
Constrained adjoint-based aerodynamic shape optimization of a single-stage transonic compressor
B Walther, S Nadarajah
Journal of turbomachinery 135 (2), 2013
442013
An adjoint method for the calculation of remote sensitivities in supersonic flow
S Nadarajah, A Jameson, JJ Alonso
AIAA paper 261, 2002, 2002
422002
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
412016
Adjoint-based aerodynamic optimization of benchmark problems
F Bisson, S Nadarajah, D Shi-Dong
52nd aerospace sciences meeting, 0412, 2014
382014
Optimum Shape Design for Unsteady Flows Using Time-accurate and Non-linear Frequency Domain Methods
SK Nadarajah, A Jameson, MS McMullen
AIAA, 2003
302003
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), 2015
262015
Laminar‐turbulent flow simulation for wind turbine profiles using the γ– transition model
P Khayatzadeh, S Nadarajah
Wind Energy 17 (6), 901-918, 2014
252014
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
252011
ILES using the correction procedure via reconstruction scheme
B Vermeire, JS Cagnone, S Nadarajah
51st AIAA aerospace sciences meeting including the new horizons forum and …, 2013
222013
Implicit nonlinear frequency-domain spectral-difference scheme for periodic Euler flow
JS Cagnone, SK Nadarajah
AIAA journal 47 (2), 361-372, 2009
222009
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Articles 1–20