Year |
Citation |
Score |
2014 |
Rallabandi A, Lei J, Han J, Azad S, Lee C. Heat Transfer Measurements in Rotating Blade–Shape Serpentine Coolant Passage With Ribbed Walls at High Reynolds Numbers Journal of Turbomachinery-Transactions of the Asme. 136: 91004. DOI: 10.1115/1.4026945 |
0.585 |
|
2012 |
Rallabandi AP, Li SJ, Han JC. Unsteady wake and coolant density effects on turbine blade film cooling using pressure sensitive paint technique Journal of Heat Transfer. 134. DOI: 10.1115/1.4006748 |
0.681 |
|
2012 |
Li S, Rallabandi AP, Han J. Influence of Unsteady Wake With Trailing Edge Coolant Ejection on Turbine Blade Film Cooling Journal of Turbomachinery-Transactions of the Asme. 134: 61026. DOI: 10.1115/1.4004883 |
0.638 |
|
2012 |
Narzary DP, Liu K, Rallabandi AP, Han J. Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique Journal of Turbomachinery-Transactions of the Asme. 134: 31006. DOI: 10.1115/1.4003025 |
0.62 |
|
2011 |
Li SJ, Rallabandi AP, Han JC. Influence of unsteady wake with trailing edge coolant ejection on turbine blade film cooling Proceedings of the Asme Turbo Expo. 5: 435-445. DOI: 10.1115/GT2011-45925 |
0.556 |
|
2011 |
Alkhamis NY, Rallabandi AP, Han JC. Heat transfer and pressure drop correlations for square channels with V-shaped ribs at high reynolds numbers Journal of Heat Transfer. 133. DOI: 10.1115/1.4004207 |
0.546 |
|
2011 |
Rallabandi AP, Liu Y, Han J. Heat Transfer in Trailing Edge Wedge-Shaped Pin-Fin Channels With Slot Ejection Under High Rotation Numbers Journal of Thermal Science and Engineering Applications. 3: 21007. DOI: 10.1115/1.4003746 |
0.541 |
|
2011 |
Rallabandi AP, Grizzle J, Han JC. Effect of upstream step on flat plate film-cooling effectiveness using PSP Journal of Turbomachinery. 133. DOI: 10.1115/1.4002422 |
0.533 |
|
2011 |
Rallabandi AP, Alkhamis N, Han JC. Heat transfer and pressure drop measurements for a square channel with 45 deg round-edged ribs at high reynolds numbers Journal of Turbomachinery. 133. DOI: 10.1115/1.4001243 |
0.545 |
|
2010 |
Han JC, Rallabandi AP. Turbine Blade Film Cooling Using PSP Technique Frontiers in Heat and Mass Transfer. 1. DOI: 10.5098/Hmt.V1.1.3001 |
0.655 |
|
2010 |
Rallabandi AP, Li SJ, Han JC. Unsteady wake and coolant density effects on turbine blade film cooling using PSP technique 2010 14th International Heat Transfer Conference, Ihtc 14. 5: 227-237. DOI: 10.1115/IHTC14-22911 |
0.61 |
|
2010 |
Rallabandi AP, Liu YH, Han JC. Heat transfer in trailing edge wedge-shaped pin-fin channels with slot ejection under high rotation numbers Proceedings of the Asme Turbo Expo. 4: 369-380. DOI: 10.1115/GT2010-22832 |
0.432 |
|
2010 |
Narzary DP, Liu KC, Rallabandi AP, Han JC. Influence of coolant density on turbine blade film-cooling using Pressure Sensitive Paint technique Proceedings of the Asme Turbo Expo. 4: 1529-1540. DOI: 10.1115/GT2010-22781 |
0.658 |
|
2010 |
Rallabandi AP, Rhee DH, Gao Z, Han JC. Heat transfer enhancement in rectangular channels with axial ribs or porous foam under through flow and impinging jet conditions International Journal of Heat and Mass Transfer. 53: 4663-4671. DOI: 10.1016/J.Ijheatmasstransfer.2010.06.027 |
0.512 |
|
2009 |
Rallabandi AP, Alkhamis N, Han JC. Heat transfer and pressure drop measurements for a square channel with 45deg round edged ribs at high Reynolds numbers Proceedings of the Asme Turbo Expo. 3: 527-538. DOI: 10.1115/GT2009-59546 |
0.427 |
|
2009 |
Rallabandi AP, Yang H, Han JC. Heat transfer and pressure drop correlations for square Channels with 45 deg ribs at high Reynolds numbers Journal of Heat Transfer. 131: 1-10. DOI: 10.1115/1.3090818 |
0.53 |
|
2009 |
Rallabandi AP, Grizzle J, Han JC. Effect of upstream step on flat plate film cooling effectiveness using PSP 2008 Proceedings of the Asme Summer Heat Transfer Conference, Ht 2008. 2: 599-609. |
0.4 |
|
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