Film cooling on a gas turbine blade pressure side or suction side with axial shaped holes Z Gao, DP Narzary, JC Han International Journal of Heat and Mass Transfer 51 (9-10), 2139-2152, 2008 | 160 | 2008 |
Influence of coolant density on turbine blade film-cooling using pressure sensitive paint technique DP Narzary, KC Liu, AP Rallabandi, JC Han | 114 | 2012 |
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip S Mhetras, D Narzary, Z Gao, JC Han | 108 | 2008 |
Turbine blade platform film cooling with typical stator-rotor purge flow and discrete-hole film cooling Z Gao, D Narzary, JC Han | 96 | 2009 |
Film-cooling on a gas turbine blade pressure side or suction side with compound angle shaped holes Z Gao, DP Narzary, JC Han | 94 | 2009 |
Experiment on gas ingestion through axial-flow turbine rim seals RP Roy, J Feng, D Narzary, RE Paolillo J. Eng. Gas Turbines Power 127 (3), 573-582, 2005 | 64 | 2005 |
Film-cooling performance of antivortex hole on a flat plate C LeBlanc, DP Narzary, S Ekkad Journal of turbomachinery 135 (6), 061009, 2013 | 51 | 2013 |
Effect of inlet flow angle on gas turbine blade tip film cooling Z Gao, D Narzary, S Mhetras, JC Han | 48 | 2009 |
Full-coverage film cooling for a turbine blade with axial-shaped holes Z Gao, DP Narzary, S Mhetras, JC Han Journal of Thermophysics and Heat Transfer 22 (1), 50-61, 2008 | 46 | 2008 |
Experiments on gas ingestion through axial-flow turbine rim seals RP Roy, J Feng, D Narzary, P Saurabh, RE Paolillo Turbo Expo: Power for Land, Sea, and Air 41693, 347-358, 2004 | 40 | 2004 |
Effect of unsteady wake on film-cooling effectiveness distribution on a gas turbine blade with compound shaped holes DP Narzary, Z Gao, S Mhetras, JC Han Turbo Expo: Power for Land, Sea, and Air 47934, 79-91, 2007 | 34 | 2007 |
Film cooling performance of tripod antivortex injection holes over the pressure and suction surfaces of a nozzle guide vane S Ramesh, C LeBlanc, D Narzary, S Ekkad, M Anne Alvin Journal of Thermal Science and Engineering Applications 9 (2), 021006, 2017 | 28 | 2017 |
Influence of coolant density on turbine blade film-cooling using pressure sensitive paint technique DP Narzary, KC Liu, AP Rallabandi, JC Han Turbo Expo: Power for Land, Sea, and Air 43994, 1529-1540, 2010 | 25 | 2010 |
Heat transfer and thermal mechanical stress distributions in gas turbine blades FZ Sierra, D Narzary, C Bolaina, JC Han, J Kubiak, J Nebradt Turbo Expo: Power for Land, Sea, and Air 48845, 115-126, 2009 | 23 | 2009 |
Turbine blade platform film cooling with typical stator-rotor purge flow and discrete-hole film cooling Z Gao, D Narzary, JC Han Turbo Expo: Power for Land, Sea, and Air 43147, 263-274, 2008 | 23 | 2008 |
Influence of shock wave on turbine vane suction side film cooling with compound-angle shaped holes K Liu, DP Narzary, JC Han, AV Mirzamoghadam, A Riahi Turbo Expo: Power for Land, Sea, and Air 54655, 447-457, 2011 | 22 | 2011 |
Upstream Vortex Effects on Turbine Blade Platform Film Cooling With Typical Purge Flow Z Gao, DP Narzary, S Mhetras, JC Han Journal of thermophysics and heat transfer 26 (1), 75-84, 2012 | 20 | 2012 |
Turbine blade tip film-cooling and heat transfer measurements at high blowing ratios D Narzary, K Liu, JC Han, S Mhetras, K Landis Turbo Expo: Power for Land, Sea, and Air 45721, V05BT13A025, 2014 | 16 | 2014 |
Influence of coolant density on turbine blade platform film-cooling DP Narzary, KC Liu, JC Han Turbo Expo: Power for Land, Sea, and Air 48845, 287-299, 2009 | 16 | 2009 |
Experimental Study of Gas Turbine Blade Film Cooling and Heat Transfer DP Narzary Texas A & M University, 2010 | 13 | 2010 |