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Andrew Corrigan
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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
298*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
772019
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
682012
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, ...
60*
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
432021
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
412016
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
382017
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
322014
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
302018
Computational Study of Shock-Associated Noise Characteristics Using LES
J Liu, A Corrigan, K Kailasanath, N Heeb, D Munday, E Gutmark
282013
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
272019
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
272016
Radial Effects on Rotating Detonation Engine Swirl
CA Nordeen, D Schwer, A Corrigan, B Cetegen
51st AIAA/SAE/ASEE Joint Propulsion Conference, 3781, 2015
272015
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
272014
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
252021
Comparison of lattice-boltzmann and finite difference solvers
R Lohner, AT Corrigan, KR Wichmann, W Wall
52nd Aerospace Sciences Meeting, 1439, 2014
242014
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
242010
Large-Eddy Simulations of Supersonic Jet Noise Generation Using Wall Modeling
J Liu, AT Corrigan
2018 AIAA/CEAS Aeroacoustics Conference, 3943, 2018
232018
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
222019
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
212019
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