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Andrew Corrigan
Andrew Corrigan
U.S. Naval Research Laboratory
Подтвержден адрес электронной почты в домене nrl.navy.mil
Название
Процитировано
Процитировано
Год
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
722019
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
392021
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
392016
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
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
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
Comparison of lattice-boltzmann and finite difference solvers
R Lohner, AT Corrigan, KR Wichmann, W Wall
52nd Aerospace Sciences Meeting, 1439, 2014
252014
Computational Study of Shock-Associated Noise Characteristics Using LES
J Liu, A Corrigan, K Kailasanath, N Heeb, D Munday, E Gutmark
252013
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
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
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
222021
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
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
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
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
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Статьи 1–20