| Running unstructured grid‐based CFD solvers on modern graphics hardware A Corrigan, FF Camelli, R Löhner, J Wallin International Journal for Numerical Methods in Fluids 66 (2), 221-229, 2010 | 295* | 2010 |
| A moving discontinuous Galerkin finite element method for flows with interfaces A Corrigan, AD Kercher, DA Kessler International Journal for Numerical Methods in Fluids 89 (9), 362-406, 2019 | 73 | 2019 |
| Semi‐automatic porting of a large‐scale Fortran CFD code to GPUs A Corrigan, F Camelli, R Löhner, F Mut International Journal for Numerical Methods in Fluids 69 (2), 314-331, 2012 | 67 | 2012 |
| Impact of Deck and Jet Blast Deflector on the Flow and Acoustic Properties of Imperfectly Expanded Supersonic Jets J Liu, A Corrigan, K Kailasanath, R Ramammurti, N Heeb, D Munday, ... | 59* | |
| The moving discontinuous Galerkin finite element method with interface condition enforcement for compressible viscous flows AD Kercher, A Corrigan, DA Kessler International Journal for Numerical Methods in Fluids 93 (5), 1490-1519, 2021 | 40 | 2021 |
| Impact of the Specific Heat Ratio On the Noise Generation in a High-Temperature Supersonic Jet J Liu, AT Corrigan, K Kailasanath, BD Taylor 54th AIAA Aerospace Sciences Meeting, 2125, 2016 | 39 | 2016 |
| Flow Statistics and Noise of Ideally Expanded Supersonic Rectangular and Circular Jets K Viswanath, R Johnson, A Corrigan, K Kailasanath, P Mora, F Baier, ... AIAA Journal 55 (10), 3425-3439, 2017 | 34 | 2017 |
| Towards efficient, unsteady, three-dimensional rotating detonation engine simulations D Schwer, A Corrigan, K K. 52nd Aerospace Sciences Meeting, AIAA SciTech, AIAA 2014-1014, 2014 | 31 | 2014 |
| Investigation of a Supersonic Jet from a Three-Stream Engine Nozzle CJ Ruscher, AS Magstadt, MG Berry, MN Glauser, PR Shea, K Viswanath, ... AIAA Journal 56 (4), 1554-1568, 2018 | 28 | 2018 |
| Noise characteristics of a rectangular vs circular nozzle for ideally expanded jet flow K Viswanath, RF Johnson, AT Corrigan, K Kailasanath, PA Mora, F Baier, ... 54th AIAA Aerospace Sciences Meeting, 1638, 2016 | 27 | 2016 |
| Numerical study of noise sources characteristics in an underexpanded jet flow J Liu, AT Corrigan, K Kailasanath, NS Heeb, EJ Gutmark 20th AIAA/CEAS Aeroacoustics Conference, 2604, 2014 | 27 | 2014 |
| Radial Effects on Rotating Detonation Engine Swirl CA Nordeen, D Schwer, A Corrigan, B Cetegen 51st AIAA/SAE/ASEE Joint Propulsion Conference, 3781, 2015 | 26 | 2015 |
| Computational Study of Shock-Associated Noise Characteristics Using LES J Liu, A Corrigan, K Kailasanath, N Heeb, D Munday, E Gutmark | 26 | 2013 |
| The Moving Discontinuous Galerkin Method with Interface Condition Enforcement for Unsteady Three-Dimensional Flows AT Corrigan, A Kercher, DA Kessler AIAA Scitech 2019 Forum, 0642, 2019 | 24 | 2019 |
| Comparison of lattice-boltzmann and finite difference solvers R Lohner, AT Corrigan, KR Wichmann, W Wall 52nd Aerospace Sciences Meeting, 1439, 2014 | 24 | 2014 |
| Porting of an edge-based CFD solver to GPUs A Corrigan, F Camelli, R Löhner, F Mut 48th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and …, 2010 | 24 | 2010 |
| A least-squares formulation of the moving discontinuous Galerkin finite element method with interface condition enforcement AD Kercher, A Corrigan Computers & Mathematics with Applications 95, 143-171, 2021 | 23 | 2021 |
| Large-Eddy Simulations of Supersonic Jet Noise Generation Using Wall Modeling J Liu, AT Corrigan 2018 AIAA/CEAS Aeroacoustics Conference, 3943, 2018 | 22 | 2018 |
| Convergence of the Moving Discontinuous Galerkin Method with Interface Condition Enforcement in the Presence of an Attached Curved Shock AT Corrigan, AD Kercher, DA Kessler, DA Wood-Thomas AIAA Aviation 2019 Forum, 3207, 2019 | 21 | 2019 |
| Progress in Efficient, High-Fidelity, Rotating Detonation Engine Simulations DA Schwer, RF Johnson, A Kercher, D Kessler, AT Corrigan AIAA Scitech 2019 Forum, 2018, 2019 | 20 | 2019 |
Kazhikathra KailasanathNaval Research LaboratoryVerified email at lcp.nrl.navy.mil
