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Paul Walsh
Paul Walsh
Verified email at ryerson.ca
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Cited by
Cited by
Year
Effectiveness of several turbulence models in natural convection
PC Walsh, WH Leong
International Journal of Numerical Methods for Heat & Fluid Flow 14 (5), 633-648, 2004
382004
Towards understanding the influence of gradient reconstruction methods on unstructured flowsimulations
F Mishriky, P Walsh
Transactions of the Canadian society for mechanical engineering 41 (2), 169-179, 2017
242017
Boundary-layer correction for the Busemann hypersonic air inlet
PC Walsh, RB Tahir, S Molder
Canadian Aeronautics and Space Journal 49 (1), 11-17, 2003
222003
Discretization Method for the Development of a Modular Morphing Wing
AD Finistauri, F Xi, P Walsh
Journal of Aircraft 49 (1), 116-125, 2012
212012
Rugged, scramjet inlet temperature and velocity sensor: design and ground test
J Kurtz, M Aizengendler, Y Krishna, P Walsh, S O’Byrne
AIAA Journal 54 (2), 399-407, 2016
192016
Flight test of a rugged scramjet-inlet temperature and velocity sensor
J Kurtz, M Aizengendler, Y Krishna, P Walsh, SB O'Byrne
53rd AIAA Aerospace Sciences Meeting, 0110, 2015
192015
Effect of the backward-facing step location on the aerodynamics of a morphing wing
F Mishriky, P Walsh
Aerospace 3 (3), 25, 2016
172016
Solution adaptation of unstructured grids for two-dimensional aerodynamic computations
PC Walsh, DW Zingg
AIAA journal 39 (5), 831-837, 2001
152001
The effect of turbulence model solution on viscous flow problems
P Walsh, T Pulliam
39th Aerospace Sciences Meeting and Exhibit, 1018, 2001
142001
Subsonic in-flight temperature and pressure measurements using a scramjet inlet flow sensor
J Kurtz, M Aizengendler, Y Krishna, P Walsh, M Brown, S O’Byrne
Aiaa Journal 54 (3), 1011-1017, 2016
102016
Adaptive solution of viscous aerodynamic flows using unstructured grids.
PC Walsh
University of Toronto, 1999
81999
Effect of Step Depth and Angle in Kline-Fogleman (KFm-2) Airfoil
F Mishriky, P Walsh
Global Journal of Researches in Engineering–J General Engineering 16 (4), 2016
62016
Early onset prediction for rotors in vortex ring state
J McQuaid, A Kolaei, G Bramesfeld, P Walsh
Journal of Aerospace Engineering 33 (6), 04020081, 2020
42020
Effect of Step Depth and Angle on the Aerodynamics of a Sliding Morphing Skin
F Mishriky, P Walsh
American Journal of Aerospace Engineering 3 (3), 24-30, 2016
42016
Aerodynamic computations using adaptive unstructured grids
PC Walsh, DW Zingg
Canadian Aeronautics and Space Journal 43 (4), 244-249, 1997
31997
On the accuracy of viscous airfoil computations using solution-adaptive unstructured grids
P Walsh, D Zingg, P Walsh, D Zingg
35th Aerospace Sciences Meeting and Exhibit, 329, 1997
21997
Wing Line Discretization for the Development of a Modular Morphing Wing
A Finistauri, F Xi, P Walsh, K Behdinan
52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2011
12011
Boundary-Layer Transition Prediction over Cavities and Its Morphing Skin Design Application
F Mishriky, PC Walsh
AIAA Journal 56 (12), 4685-4696, 2018
2018
Module discretization and consolidation of a modular morphing wing
R Perera, P Paudel, J Kamel, F Xi, P Walsh
Canadian Aeronautics and Space Journal 61 (2), 36-50, 2015
2015
Numerical study of bleed slot flow characteristics using magneto-aerodynamics
S Buhajczuk, P Walsh
International Journal of Computational Fluid Dynamics 22 (1-2), 11-18, 2008
2008
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Articles 1–20