Explicit Runge-Kutta method for unsteady rotor/stator interaction PCE Jorgenson, RV Chima AIAA journal 27 (6), 743-749, 1989 | 79 | 1989 |
Mixed phase modeling in GlennICE with application to engine icing W Wright, P Jorgenson, J Veres AIAA Atmospheric and Space Environments Conference, 7674, 2010 | 67 | 2010 |
Central difference TVD schemes for time dependent and steady state problems P Jorgenson, E Turkel Journal of Computational Physics 107 (2), 297-308, 1993 | 60 | 1993 |
An unconditionally stable Runge-Kutta method for unsteady flows P JORGENSON, R CHIMA 27th Aerospace Sciences Meeting, 205, 1989 | 58 | 1989 |
Robust and simple non-reflecting boundary conditions for the space-time conservation element and solution element method SC Chang, C Loh, ST Yu, A Himansu, XY Wang, P Jorgenson, SC Chang, ... 13th Computational Fluid Dynamics Conference, 2077, 1997 | 50 | 1997 |
Modeling commercial turbofan engine icing risk with ice crystal ingestion JP Veres, PC Jorgenson 5th AIAA Atmospheric and Space Environments Conference, 2679, 2013 | 47 | 2013 |
Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method C Loh, L Hultgren, P Jorgenson 7th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2252, 2001 | 47 | 2001 |
Computing axisymmetric jet screech tones using unstructured grids P Jorgenson, C Loh 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3889, 2002 | 39 | 2002 |
A mixed volume grid approach for the Euler and Navier-Stokes equations W Coirier, P Jorgenson 34th Aerospace Sciences Meeting and Exhibit, 762, 1996 | 37 | 1996 |
Accuracy study of the space-time CE/SE method for computational aeroacoustics problems involving shock waves XY Wang, SC Chang, P Jorgenson 38th Aerospace Sciences Meeting and Exhibit, 474, 1999 | 31 | 1999 |
Modeling of Highly Instrumented Honeywell Turbofan Engine Tested with Ice Crystal Ingestion in the NASA Propulsion System Laboratory JP Veres, P Jorgenson, SM Jones 8th AIAA Atmospheric and Space Environments Conference, 3895, 2016 | 29 | 2016 |
A model to assess the risk of ice accretion due to ice crystal ingestion in a turbofan engine and its effects on performance J Veres, P Jorgenson, W Wright 4th AIAA atmospheric and space environments conference, 3038, 2012 | 28 | 2012 |
Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method CY Loh, SC Chang, PCE Jorgenson, LS Hultgren AIAA, Aerospace Sciences Meeting and Exhibit, 38 th, Reno, NV, 2000 | 27 | 2000 |
Application of the CESE method to detonation with realistic finite-rate chemistry KS Im, ST Joh, CK Kim, SC Chang, C Jorgenson 40th AIAA Aerospace Sciences Meeting & Exhibit, 1020, 2002 | 25 | 2002 |
Prediction of sound waves propagating through a nozzle without/with a shock wave using the space-time CE/SE method XY Wang, SC Chang, P Jorgenson 38th Aerospace Sciences Meeting and Exhibit, 222, 2000 | 25 | 2000 |
A modified space-time conservation element and solution element method for Euler and Navier-Stokes equations ZC Zhang, S Yu, SC Chang, A Himansu, P Jorgenson 14th Computational Fluid Dynamics Conference, 3277, 1999 | 25 | 1999 |
Vortex dynamics simulation in aeroacoustics by the space-time conservation element and solution element method C Loh, L Hultgren, SC Chang, P Jorgenson 37th Aerospace Sciences Meeting and Exhibit, 359, 1999 | 25 | 1999 |
Treating stiff source terms in conservation laws by the space-time conservation element and solution element method ST Yu, SC Chang, PCE Jorgenson, SJ Park, MC Lai Sixteenth International Conference on Numerical Methods in Fluid Dynamics …, 1998 | 25 | 1998 |
The CE/SE method for Navier-Stokes equations using unstructured meshes for flows at all speeds ZC Zhang, S Yu, XY Wang, SC Chang, A Himansu, P Jorgenson 38th Aerospace Sciences Meeting and Exhibit, 393, 2000 | 24 | 2000 |
Engine icing modeling and simulation (part I): Ice crystal accretion on compression system components and modeling its effects on engine performance PCE Jorgenson, JP Veres, WB Wright, RD May SAE Technical Paper, 2011 | 23 | 2011 |