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Philip Jorgenson
Philip Jorgenson
Aerospace Engineer, NASA
在 nasa.gov 的电子邮件经过验证
标题
引用次数
引用次数
年份
Explicit Runge-Kutta method for unsteady rotor/stator interaction
PCE Jorgenson, RV Chima
AIAA journal 27 (6), 743-749, 1989
791989
Mixed phase modeling in GlennICE with application to engine icing
W Wright, P Jorgenson, J Veres
AIAA Atmospheric and Space Environments Conference, 7674, 2010
672010
Central difference TVD schemes for time dependent and steady state problems
P Jorgenson, E Turkel
Journal of Computational Physics 107 (2), 297-308, 1993
601993
An unconditionally stable Runge-Kutta method for unsteady flows
P JORGENSON, R CHIMA
27th Aerospace Sciences Meeting, 205, 1989
581989
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
501997
Modeling commercial turbofan engine icing risk with ice crystal ingestion
JP Veres, PC Jorgenson
5th AIAA Atmospheric and Space Environments Conference, 2679, 2013
472013
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
472001
Computing axisymmetric jet screech tones using unstructured grids
P Jorgenson, C Loh
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3889, 2002
392002
A mixed volume grid approach for the Euler and Navier-Stokes equations
W Coirier, P Jorgenson
34th Aerospace Sciences Meeting and Exhibit, 762, 1996
371996
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
311999
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
292016
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
282012
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
272000
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
252002
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
252000
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
251999
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
251999
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
251998
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
242000
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
232011
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