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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
289*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
702019
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*
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
382016
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
372021
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
312017
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
312014
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
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
Radial Effects on Rotating Detonation Engine Swirl
CA Nordeen, D Schwer, A Corrigan, B Cetegen
51st AIAA/SAE/ASEE Joint Propulsion Conference, 3781, 2015
252015
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
242018
Comparison of lattice-boltzmann and finite difference solvers
R Lohner, AT Corrigan, KR Wichmann, W Wall
52nd Aerospace Sciences Meeting, 1439, 2014
242014
Computational Study of Shock-Associated Noise Characteristics Using LES
J Liu, A Corrigan, K Kailasanath, N Heeb, D Munday, E Gutmark
242013
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
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
222019
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
212021
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
202019
Area effects on rotating detonation engine performance
CA Nordeen, D Schwer, A Corrigan
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3900, 2014
202014
Large-Eddy Simulations of Supersonic Jet Noise Generation Using Wall Modeling
J Liu, AT Corrigan
2018 AIAA/CEAS Aeroacoustics Conference, 3943, 2018
192018
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