| Year |
Citation |
Score |
| 2015 |
Otto M, Hodges JD, Kapat JS, Mhetras S, Ricklick MA. Combination of ribs and pins for internal cooling 51st Aiaa/Sae/Asee Joint Propulsion Conference. |
0.316 |
|
| 2014 |
Narzary D, Liu K, Han JC, Mhetras S, Landis K. Turbine blade tip film-cooling and heat transfer measurements at high blowing ratios Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2014-25793 |
0.666 |
|
| 2014 |
Mhetras S, Han JC, Huth M. Heat transfer and pressure loss measurements in a turbulated high aspect ratio channel with large reynolds number flows Journal of Thermal Science and Engineering Applications. 6. DOI: 10.1115/1.4027299 |
0.449 |
|
| 2013 |
Mhetras S, Han JC, Huth M. Impingement heat transfer from jet arrays on turbulated target walls at large Reynolds numbers Journal of Thermal Science and Engineering Applications. 6. DOI: 10.1115/1.4025665 |
0.476 |
|
| 2012 |
Gao Z, Narzary DP, Mhetras S, Han JC. Upstream vortex effect on turbine platform film cooling with typical purge flow Journal of Thermophysics and Heat Transfer. 26: 75-84. DOI: 10.2514/1.42411 |
0.784 |
|
| 2011 |
Mhetras S, Han JC, Rudolph R. Effect of flow parameter variations on full coverage film-cooling effectiveness for a gas turbine blade Journal of Turbomachinery. 134. DOI: 10.1115/1.4003228 |
0.678 |
|
| 2009 |
Gao Z, Narzary D, Mhetras S, Han JC. Effect of inlet flow angle on gas turbine blade tip film cooling Journal of Turbomachinery. 131. DOI: 10.1115/1.2987235 |
0.797 |
|
| 2009 |
Suryanarayanan A, Mhetras SP, Schobeiri MT, Han JC. Film-cooling effectiveness on a rotating blade platform Journal of Turbomachinery. 131. DOI: 10.1115/1.2752184 |
0.722 |
|
| 2008 |
Gao Z, Narzary DP, Mhetras S, Han JC. Full-coverage film cooling for a turbine blade with axial-shaped holes Journal of Thermophysics and Heat Transfer. 22: 50-61. DOI: 10.2514/1.31206 |
0.801 |
|
| 2008 |
Gao Z, Narzary D, Mhetras S, Han JC. Upstream vortex effects on turbine blade platform film cooling with typical stator-rotor purge flow Asme International Mechanical Engineering Congress and Exposition, Proceedings. 8: 707-718. DOI: 10.1115/IMECE2007-41717 |
0.765 |
|
| 2008 |
Mhetras S, Han JC, Rudolph R. Film-cooling effectiveness from shaped film cooling holes for a gas turbine blade Proceedings of the Asme Turbo Expo. 4: 837-848. DOI: 10.1115/GT2008-50916 |
0.689 |
|
| 2008 |
Choi JH, Mhetras S, Han JC, Lau SC, Rudolph R. Film cooling and heat transfer on two cutback trailing edge models with internal perforated blockages Journal of Heat Transfer. 130. DOI: 10.1115/1.2780174 |
0.642 |
|
| 2008 |
Mhetras S, Narzary D, Gao Z, Han JC. Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip Journal of Turbomachinery. 130. DOI: 10.1115/1.2776949 |
0.799 |
|
| 2007 |
Narzary DP, Gao Z, Mhetras S, Han JC. Effect of unsteady wake on film-cooling effectiveness distribution on a gas turbine blade with compound shaped holes Proceedings of the Asme Turbo Expo. 4: 79-91. DOI: 10.1115/GT2007-27070 |
0.811 |
|
| 2007 |
Gao Z, Narzary DP, Mhetras S, Han JC. Full coverage film cooling for a turbine blade with axial shaped holes Collection of Technical Papers - 39th Aiaa Thermophysics Conference. 1: 180-193. |
0.822 |
|
| 2006 |
Mhetras S, Yang H, Gao Z, Han J. Film-Cooling Effectiveness on Squealer Cavity and Rim Walls of Gas-Turbine Blade Tip Journal of Propulsion and Power. 22: 889-899. DOI: 10.2514/1.19201 |
0.853 |
|
| 2006 |
Mhetras S, Han JC. Effect of superposition on spanwise film-cooling effectiveness distribution on a gas turbine blade American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. DOI: 10.1115/IMECE2006-15084 |
0.835 |
|
| 2006 |
Mhetras S, Narzary D, Gao Z, Han JC. Effect of a cutback squealer and cavity depth on film-cooling effectiveness for a gas turbine blade tip Collection of Technical Papers - 9th Aiaa/Asme Joint Thermophysics and Heat Transfer Conference Proceedings. 2: 1399-1413. |
0.829 |
|
| 2006 |
Mhetras S, Yang H, Gao Z, Han JC. Film-cooling effectiveness on squealer cavity and rim walls of gas-turbine blade tip Journal of Propulsion and Power. 22: 889-899. |
0.831 |
|
| 2006 |
Mhetras S, Han JC. Effect of unsteady wake on full coverage film-cooling effectiveness for a gas turbine blade Collection of Technical Papers - 9th Aiaa/Asme Joint Thermophysics and Heat Transfer Conference Proceedings. 2: 1382-1398. |
0.852 |
|
| 2005 |
Mhetras S, Yang H, Gao Z, Han JC. Film-cooling effectiveness on squealer rim walls and squealer cavity floor of a gas turbine blade tip using pressure sensitive paint Proceedings of the Asme Turbo Expo. 3: 397-408. DOI: 10.1115/GT2005-68387 |
0.834 |
|
| 2005 |
Ahn J, Mhetras S, Han JC. Film-cooling effectiveness on a gas turbine blade tip using pressure-sensitive paint Journal of Heat Transfer. 127: 521-530. DOI: 10.1115/1.1909208 |
0.83 |
|
| 2004 |
Ahn J, Mhetras S, Han JC. Film-cooling effectiveness on a gas turbine blade tip using pressure sensitive paint Proceedings of the Asme Turbo Expo 2004. 3: 241-250. |
0.795 |
|
| 2002 |
Mhetras S, Lau SC. Experiments on effect of jet impingement on heat transfer in annular channels with parallel and counter flows American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. 372: 39-48. DOI: 10.1115/IMECE2002-33658 |
0.359 |
|
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