| Turbomachinery flow physics and dynamic performance M Schobeiri Springer, 2005 | 313 | 2005 |
| GETRAN: A generic, modularly structured computer code for simulation of dynamic behavior of aero-and power generation gas turbine engines MT Schobeiri, M Attia, C Lippke | 154 | 1994 |
| Fluid mechanics for engineers: a graduate textbook MT Schobeiri Springer Science & Business Media, 2010 | 115 | 2010 |
| Five-hole pressure probe analysis technique GL Morrison, MT Schobeiri, KR Pappu Flow measurement and Instrumentation 9 (3), 153-158, 1998 | 114 | 1998 |
| Film-cooling effectiveness on a rotating blade platform A Suryanarayanan, SP Mhetras, MT Schobeiri, JC Han | 96 | 2009 |
| Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes J Ahn, MT Schobeiri, JC Han, HK Moon International Journal of Heat and Mass Transfer 50 (1-2), 15-25, 2007 | 96 | 2007 |
| On the physics of flow separation along a low pressure turbine blade under unsteady flow conditions MT Schobeiri, B Öztürk, DE Ashpis | 94 | 2005 |
| Film-cooling effectiveness on a rotating turbine platform using pressure sensitive paint technique A Suryanarayanan, B Ozturk, MT Schobeiri, JC Han | 92 | 2010 |
| Effect of unsteady wake passing frequency on boundary layer transition, experimental investigation, and wavelet analysis MT Schobeiri, K Read, J Lewalle J. Fluids Eng. 125 (2), 251-266, 2003 | 76* | 2003 |
| A combined experimental and numerical study of the turbine blade tip film cooling effectiveness under rotation condition M Rezasoltani, K Lu, MT Schobeiri, JC Han Journal of Turbomachinery 137 (5), 051009, 2015 | 73 | 2015 |
| Experimental study of the effect of periodic unsteady wake flow on boundary layer development, separation, and reattachment along the surface of a low pressure turbine blade MT Schobeiri, B O¨ ztu¨ rk J. Turbomach. 126 (4), 663-676, 2004 | 73 | 2004 |
| Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint J Ahn, MT Schobeiri, JC Han, HK Moon | 72 | 2006 |
| Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model MT Schobeiri, P Chakka International Journal of Heat and Mass Transfer 45 (4), 815-829, 2002 | 56 | 2002 |
| Gas turbine design, components and system design integration: second revised and enhanced edition MT Schobeiri Springer Nature, 2019 | 54 | 2019 |
| Film cooling effectiveness on the leading edge of a rotating film-cooled blade using pressure sensitive paint J Ahn, MT Schobeiri, JC Han, HK Moon Turbo Expo: Power for Land, Sea, and Air 47268, 375-384, 2005 | 53 | 2005 |
| Modeling unsteady boundary layer transition on a curved plate under periodic unsteady flow conditions: Aerodynamic and heat transfer investigations P Chakka, MT Schobeiri | 51 | 1999 |
| A comparative aerodynamic and performance study of a three-stage high pressure turbine with 3-D bowed blades and cylindrical blades MT Schobeiri, A Suryanarayanan, C Jermann, T Neuenschwander Turbo Expo: Power for Land, Sea, and Air 41707, 1237-1246, 2004 | 50 | 2004 |
| Film cooling effectiveness on the leading edge of a rotating turbine blade J Ahn, MT Schobeiri, JC Han, HK Moon ASME International Mechanical Engineering Congress and Exposition 4711, 565-574, 2004 | 50 | 2004 |
| Aerodynamic and performance studies of a three-stage high pressure research turbine with 3-D-blades, design point and off-design experimental investigations MT Schobeiri, JL Gilarranz, ES Johansen Turbo Expo: Power for Land, Sea, and Air 78545, V001T03A054, 2000 | 49 | 2000 |
| The effect of periodic unsteady flow on aerodynamics and heat transfer on a curved surface L Wright, MT Schobeiri | 49 | 1999 |
