| Adaptive remeshing for compressible flow computations J Peraire, M Vahdati, K Morgan, OC Zienkiewicz Journal of computational physics 72 (2), 449-466, 1987 | 1374 | 1987 |
| Finite element flux‐corrected transport (FEM–FCT) for the euler and Navier–Stokes equations R Löhner, K Morgan, J Peraire, M Vahdati International Journal for Numerical Methods in Fluids 7 (10), 1093-1109, 1987 | 520 | 1987 |
| An integrated nonlinear approach for turbomachinery forced response prediction. Part I: Formulation AI Sayma, M Vahdati, M Imregun Journal of fluids and structures 14 (1), 87-101, 2000 | 189* | 2000 |
| Modeling of three-dimensional viscous compressible turbomachinery flows using unstructured hybrid grids AI Sayma, M Vahdati, L Sbardella, M Imregun AIAA journal 38 (6), 945-954, 2000 | 171 | 2000 |
| Rotating stall observations in a high speed compressor—Part II: Numerical study J Dodds, M Vahdati Journal of Turbomachinery 137 (5), 051003, 2015 | 160* | 2015 |
| On the use of atmospheric boundary conditions for axial-flow compressor stall simulations M Vahdati, AI Sayma, C Freeman, M Imregun | 147 | 2005 |
| FEM‐FCT: combining unstructured grids with high resolution R Löhner, K Morgan, M Vahdati, JP Boris, DL Book Communications in Applied Numerical Methods 4 (6), 717-729, 1988 | 135 | 1988 |
| Mechanisms for wide-chord fan blade flutter M Vahdati, G Simpson, M Imregun | 113 | 2011 |
| Mechanisms and prediction methods for fan blade stall flutter M Vahdati, AI Sayma, JG Marshall, M Imregun Journal of Propulsion and Power 17 (5), 1100-1108, 2001 | 100 | 2001 |
| Validation of numerical simulation for rotating stall in a transonic fan M Choi, NHS Smith, M Vahdati Journal of turbomachinery 135 (2), 021004, 2013 | 95 | 2013 |
| Aeroelastic instability in transonic fans M Vahdati, N Cumpsty journal of Engineering for Gas Turbines and Power 138 (2), 022604, 2016 | 92 | 2016 |
| Effects of fan speed on rotating stall inception and recovery M Choi, M Vahdati, M Imregun | 78 | 2011 |
| Unsteady flow and aeroelasticity behavior of aeroengine core compressors during rotating stall and surge M Vahdati, G Simpson, M Imregun | 74 | 2008 |
| Validation of a numerical model for predicting stalled flows in a low-speed fan—part I: Modification of Spalart–Allmaras turbulence model KB Lee, M Wilson, M Vahdati Journal of Turbomachinery 140 (5), 051008, 2018 | 70 | 2018 |
| Influence of the inlet distortion on fan stall margin at different rotational speeds W Zhang, S Stapelfeldt, M Vahdati Aerospace Science and Technology 98, 105668, 2020 | 65 | 2020 |
| A parametric study of the effects of inlet distortion on fan aerodynamic stability W Zhang, M Vahdati Journal of Turbomachinery 141 (1), 011011, 2019 | 64 | 2019 |
| Influence of intake on fan blade flutter M Vahdati, N Smith, F Zhao Journal of Turbomachinery 137 (8), 081002, 2015 | 61 | 2015 |
| Multibladerow forced response modeling in axial-flow core compressors M Vahdati, AI Sayma, M Imregun, G Simpson | 55 | 2007 |
| An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion C Bre´ ard, M Vahdati, AI Sayma, M Imregun J. Eng. Gas Turbines Power 124 (1), 196-208, 2002 | 54 | 2002 |
| Spectral proper orthogonal decomposition of compressor tip leakage flow X He, Z Fang, G Rigas, M Vahdati Physics of Fluids 33 (10), 2021 | 48 | 2021 |
