Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits M Gritsch, A Schulz, S Wittig | 637 | 1998 |
Flowfield measurements for film-cooling holes with expanded exits K Thole, M Gritsch, A Schulz, S Wittig | 409 | 1998 |
Effect of hole geometry on the thermal performance of fan-shaped film cooling holes M Gritsch, W Colban, H Schär, K Döbbeling | 308 | 2005 |
Discharge coefficient measurements of film-cooling holes with expanded exits M Gritsch, A Schulz, S Wittig | 223 | 1998 |
Film-cooling holes with expanded exits: near-hole heat transfer coefficients M Gritsch, A Schulz, S Wittig International Journal of Heat and Fluid Flow 21 (2), 146-155, 2000 | 178 | 2000 |
Effect of internal coolant crossflow on the effectiveness of shaped film-cooling holes M Gritsch, A Schulz, S Wittig J. Turbomach. 125 (3), 547-554, 2003 | 160 | 2003 |
Effect of a Crossflow at the Entrance to a Film-Cooling Hole KA Thole, M Gritsch, A Schulz, S Wittig | 154 | 1997 |
Effect of crossflows on the discharge coefficient of film cooling holes with varying angles of inclination and orientation M Gritsch, A Schulz, S Wittig Turbo Expo: Power for Land, Sea, and Air 78521, V003T01A020, 2001 | 145 | 2001 |
Effect of internal coolant crossflow orientation on the discharge coefficient of shaped film-cooling holes M Gritsch, C Saumweber, A Schulz, S Wittig, E Sharp J. Turbomach. 122 (1), 146-152, 2000 | 143 | 2000 |
Heat transfer coefficient measurements of film-cooling holes with expanded exits M Gritsch, A Schulz, S Wittig Turbo Expo: Power for Land, Sea, and Air 78651, V004T09A004, 1998 | 115 | 1998 |
Transonic film-cooling investigations: effects of hole shapes and orientations S Wittig, A Schulz, M Gritsch, KA Thole Turbo Expo: Power for Land, Sea, and Air 78750, V004T09A026, 1996 | 105 | 1996 |
Method for correlating discharge coefficients of film-cooling holes M Gritsch, A Schulz, S Wittig AIAA journal 36 (6), 976-980, 1998 | 82 | 1998 |
In situ calibration for quantitative infrared thermography M Martiny, R Schiele, M Gritsch, A Schulz, S Wittig QIRT 96, 3-8, 1996 | 78 | 1996 |
The superposition approach to local heat transfer coefficients in high density ratio film cooling flows M Gritsch, S Baldauf, M Martiny, A Schulz, S Wittig Turbo Expo: Power for Land, Sea, and Air 78606, V003T01A048, 1999 | 61 | 1999 |
An experimental and numerical study of heat transfer and pressure losses of V-and W-shaped ribs at high Reynolds numbers M Maurer, J von Wolfersdorf, M Gritsch Turbo Expo: Power for Land, Sea, and Air 47934, 219-228, 2007 | 51 | 2007 |
Design considerations and validation of trailing edge pressure side bleed cooling J Krueckels, M Gritsch, M Schnieder Turbo Expo: Power for Land, Sea, and Air 48845, 63-70, 2009 | 43 | 2009 |
An experimental and numerical study of heat transfer and pressure loss in a rectangular channel with v-shaped ribs M Maurer, J von Wolfersdorf, M Gritsch | 38 | 2007 |
Effects of entrance crossflow directions to film cooling holes C Saumweber, A Schulz, S Wittig, M Gritsch Annals of the New York Academy of Sciences 934 (1), 401-408, 2001 | 38 | 2001 |
Multirow film cooling performances of a high lift blade and vane S Naik, J Krueckels, M Gritsch, M Schnieder Journal of Turbomachinery 136 (5), 051003, 2014 | 27 | 2014 |
Film-cooling from holes with expanded exits: A comparison of computational results with experiments D Giebert, M Gritsch, A Schulz, S Wittig Turbo Expo: Power for Land, Sea, and Air 78705, V003T09A028, 1997 | 26 | 1997 |