| 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 | 40 | 2004 |
| 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 | 28 | 2017 |
| Discretization Method for the Development of a Modular Morphing Wing AD Finistauri, F Xi, P Walsh Journal of Aircraft 49 (1), 116-125, 2012 | 24 | 2012 |
| 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 | 22 | 2003 |
| 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 | 21 | 2016 |
| Effect of the backward-facing step location on the aerodynamics of a morphing wing F Mishriky, P Walsh Aerospace 3 (3), 25, 2016 | 20 | 2016 |
| 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 | 18 | 2015 |
| Solution adaptation of unstructured grids for two-dimensional aerodynamic computations PC Walsh, DW Zingg AIAA journal 39 (5), 831-837, 2001 | 15 | 2001 |
| The effect of turbulence model solution on viscous flow problems P Walsh, T Pulliam 39th Aerospace Sciences Meeting and Exhibit, 1018, 2001 | 15 | 2001 |
| 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 | 13 | 2016 |
| Effect of Step Depth and Angle in Kline-Fogleman (KFm-2) Airfoil F Mishriky, P Walsh Global Journal of Research in Engineering 16 (4), 1-8, 2016 | 10 | 2016 |
| 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 | 9 | 2020 |
| Adaptive solution of viscous aerodynamic flows using unstructured grids PC Walsh | 9 | 1998 |
| 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 | 5 | 2016 |
| Early on-set prediction of vortex-ring state of quadrotors J McQuaid, A Kolaei, G Bramesfeld, P Walsh J. Aerosp. Eng 33 (6), 2020 | 3 | 2020 |
| Aerodynamic computations using adaptive unstructured grids PC Walsh, DW Zingg Canadian Aeronautics and Space Journal 43 (4), 244-249, 1997 | 3 | 1997 |
| 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 | 2 | 2011 |
| 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 | 2 | 1997 |
| 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 |
