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Diganta Narzary
Elliott Group - / United States
Engineering & Technology / Mechanical Engineering
AD Scientific Index ID: 4985808
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Diganta Narzary's MOST POPULAR ARTICLES
1-)
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 1312008
2-)
Influence of coolant density on turbine blade film-cooling using pressure sensitive paint techniqueDP Narzary, KC Liu, AP Rallabandi, JC Han932012
3-)
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tipS Mhetras, D Narzary, Z Gao, JC Han992008
4-)
Turbine blade platform film cooling with typical stator-rotor purge flow and discrete-hole film coolingZ Gao, D Narzary, JC Han962009
5-)
Film-cooling on a gas turbine blade pressure side or suction side with compound angle shaped holesZ Gao, DP Narzary, JC Han912009
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