Je-Chin Han - Publications

Affiliations: 
Mechanical Engineering Texas A & M University, College Station, TX, United States 
Area:
Mechanical Engineering

64 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2014 Wright LM, Han J. Heat Transfer Enhancement For Turbine Blade Internal Cooling Journal of Enhanced Heat Transfer. 21: 111-140. DOI: 10.1615/Jenhheattransf.2015012169  0.511
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  0.734
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  0.775
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  0.717
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  0.766
2012 Lei J, Han JC, Huh M. Effect of rib spacing on heat transfer in a two pass rectangular channel (AR 2:1) at high rotation numbers Journal of Heat Transfer. 134. DOI: 10.1115/1.4006298  0.681
2012 Narzary DP, Liu K, Han J. Influence of Coolant Density on Turbine Blade Platform Film-Cooling Journal of Thermal Science and Engineering Applications. 4: 21002. DOI: 10.1115/1.4005732  0.72
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  0.768
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  0.774
2012 Liu YH, Huh M, Han JC. High rotation number effect on heat transfer in a trailing edge channel with tapered ribs International Journal of Heat and Fluid Flow. 33: 182-192. DOI: 10.1016/J.Ijheatfluidflow.2011.10.002  0.606
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  0.765
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  0.752
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  0.7
2011 Huh M, Lei J, Han JC. Influence of channel orientation on heat transfer in a two-pass smooth and ribbed rectangular channel (AR=2:1) under large rotation numbers Journal of Turbomachinery. 134. DOI: 10.1115/1.4003172  0.673
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  0.764
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  0.76
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  0.761
2010 Liu Y, Huh M, Han J, Moon H. High Rotation Number Effect on Heat Transfer in a Triangular Channel With 45 deg, Inverted 45 deg, and 90 deg Ribs Journal of Heat Transfer-Transactions of the Asme. 132: 71702. DOI: 10.1115/1.4000986  0.333
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  0.762
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  0.758
2009 Gao Z, Narzary D, Han J. Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling Journal of Turbomachinery-Transactions of the Asme. 131: 41004. DOI: 10.1115/1.3068327  0.73
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  0.796
2009 Wright LM, Blake SA, Rhee DH, Han JC. Effect of upstream wake with vortex on turbine blade platform film cooling with simulated stator-rotor purge flow Journal of Turbomachinery. 131. DOI: 10.1115/1.2952365  0.545
2009 Gao Z, Narzary DP, Han JC. Film-cooling on a gas turbine blade pressure side or suction side with compound angle shaped holes Journal of Turbomachinery. 131. DOI: 10.1115/1.2813012  0.744
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  0.792
2008 Liu YH, Huh M, Han JC, Chopra S. Heat transfer in a two-pass rectangular channel (AR=1:4) under high rotation numbers Journal of Heat Transfer. 130. DOI: 10.1115/1.2909615  0.593
2008 Wright LM, Gao Z, Yang H, Han JC. Film cooling effectiveness distribution on a gas turbine blade platform with inclined slot leakage and discrete film hole flows Journal of Heat Transfer. 130. DOI: 10.1115/1.2907440  0.535
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  0.734
2008 Wright LM, Blake SA, Han JC. Film cooling effectiveness distributions on a turbine blade cascade platform with stator-rotor purge and discrete film hole flows Journal of Turbomachinery. 130. DOI: 10.1115/1.2777186  0.553
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  0.795
2008 Gao Z, Narzary DP, Han JC. Film cooling on a gas turbine blade pressure side or suction side with axial shaped holes International Journal of Heat and Mass Transfer. 51: 2139-2152. DOI: 10.1016/J.Ijheatmasstransfer.2007.11.010  0.744
2007 Wright LM, Blake S, Han JC. Effectiveness distributions on turbine-blade cascade platforms through simulated stator-rotor seals Journal of Thermophysics and Heat Transfer. 21: 754-762. DOI: 10.2514/1.30382  0.564
2007 Liu YH, Wright LM, Fu WL, Han JC. Rib spacing effect on heat transfer in rotating two-pass ribbed channel (AR = 1:2) Journal of Thermophysics and Heat Transfer. 21: 582-595. DOI: 10.2514/1.29128  0.703
2006 Fu WL, Wright LM, Han JC. Heat transfer in two-pass rotating rectangular channels (AR = 2:1) with discrete ribs Journal of Thermophysics and Heat Transfer. 20: 569-582. DOI: 10.2514/1.19468  0.671
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  0.728
2006 Fu WL, Wright LM, Han JC. Rotational buoyancy effects on heat transfer in five different aspect-ratio rectangular channels with smooth walls and 45 degree ribbed walls Journal of Heat Transfer. 128: 1130-1141. DOI: 10.1115/1.2352782  0.67
2005 Al-Qahtani MS, Chen H, Han J. Heat Transfer Prediction of Rotating Rectangular Channels Using Reynolds Stress Model Journal of Thermophysics and Heat Transfer. 19: 36-47. DOI: 10.2514/1.7300  0.774
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  0.727
2005 Wright LM, Fu WL, Han JC. Influence of entrance geometry on heat transfer in rotating rectangular cooling channels (AR=4:1) with angled ribs Journal of Heat Transfer. 127: 378-387. DOI: 10.1115/1.1860564  0.676
2005 Fu WL, Wright LM, Han JC. Heat transfer in two-pass rotating rectangular channels (AR=1:2 and AR=1:4) with smooth walls Journal of Heat Transfer. 127: 265-277. DOI: 10.1115/1.1857946  0.655
2005 Fu WL, Wright LM, Han JC. Heat transfer in two-pass rotating rectangular channels (AR=1:2 and AR=1:4) with 45 deg angled rib turbulators Journal of Turbomachinery. 127: 164-174. DOI: 10.1115/1.1791649  0.671
2004 Su G, Teng S, Chen H, Han J. Flow and Heat-Transfer Computations in Rotating Rectangular Channels with V-Shaped Ribs Journal of Thermophysics and Heat Transfer. 18: 534-547. DOI: 10.2514/1.8806  0.524
2004 Wright LM, Lee E, Han J. Effect of rotation on heat transfer in rectangular channels with pin fins Journal of Thermophysics and Heat Transfer. 18: 263-272. DOI: 10.2514/1.4723  0.548
2004 Wright LM, Fu WL, Han JC. Thermal performance of angled, V-shaped, and W-shaped rib turbulators in rotating rectangular cooling channels (AR=4:1) Journal of Turbomachinery. 126: 604-614. DOI: 10.1115/1.1791286  0.679
2004 Choi J, Teng S, Han JC, Ladeinde F. Effect of free-stream turbulence on turbine blade heat transfer and pressure coefficients in low Reynolds number flows International Journal of Heat and Mass Transfer. 47: 3441-3452. DOI: 10.1016/J.Ijheatmasstransfer.2004.01.015  0.537
2003 Al-Qahtani M, Chen H, Han J. A Numerical Study of Flow and Heat Transfer in Rotating Rectangular Channels (AR=4) With 45 deg Rib Turbulators by Reynolds Stress Turbulence Model Journal of Heat Transfer-Transactions of the Asme. 125: 19-26. DOI: 10.1115/1.1527907  0.774
2002 Azad GS, Huang Y, Han J. Jet Impingement Heat Transfere on Pinned Surface Using a Transient Liquid Cristal Technique International Journal of Rotating Machinery. 8: 161-173. DOI: 10.1155/S1023621X02000155  0.775
2002 Azad GS, Han J, Bunker RS, Lee CP. Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer Journal of Heat Transfer-Transactions of the Asme. 124: 452-459. DOI: 10.1115/1.1471523  0.786
2002 Azad GS, Uddin MJ, Han J, Moon H, Glezer B. Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators Journal of Turbomachinery-Transactions of the Asme. 124: 251-259. DOI: 10.1115/1.1450569  0.797
2002 Al-Qahtani M, Jang Y, Chen H, Han J. Prediction of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels With 45-deg Rib Turbulators Journal of Turbomachinery-Transactions of the Asme. 124: 242-250. DOI: 10.1115/1.1450568  0.796
2002 Azad G, Huang Y, Han J. Jet Impingement Heat Transfer on Pinned Surfaces Using a Transient Liquid Crystal Technique International Journal of Rotating Machinery. 8: 161-173. DOI: 10.1080/1023-620291910798  0.775
2002 Al-Qahtani M, Jang Y, Chen H, Han J. Flow and heat transfer in rotating two-pass rectangular channels (AR=2) by Reynolds stress turbulence model International Journal of Heat and Mass Transfer. 45: 1823-1838. DOI: 10.1016/S0017-9310(01)00292-7  0.795
2001 Teng S, Han J, Poinsatte PE. Effect of Film-Hole Shape on Turbine-Blade Film-Cooling Performance Journal of Thermophysics and Heat Transfer. 15: 257-265. DOI: 10.2514/2.6621  0.517
2001 Teng S, Han J, Poinsatte PE. Effect of Film-Hole Shape on Turbine-Blade Heat-Transfer Coefficient Distribution Journal of Thermophysics and Heat Transfer. 15: 249-256. DOI: 10.2514/2.6610  0.521
2001 Jang Y, Chen H, Han J. Numerical Prediction of Flow and Heat Transferin a Two-pass Square Channel with 90° Ribs International Journal of Rotating Machinery. 7: 195-208. DOI: 10.1155/S1023621X01000185  0.528
2001 Teng S, Han J, Azad GMS. Detailed heat transfer coefficient distributions on a large-scale gas turbine blade tip Journal of Heat Transfer-Transactions of the Asme. 123: 803-809. DOI: 10.1115/1.1373655  0.508
2001 Jang Y, Chen H, Han J. Computation of Flow and Heat Transfer in Two-Pass Channels With 60 deg Ribs Journal of Heat Transfer-Transactions of the Asme. 123: 563-575. DOI: 10.1115/1.1371931  0.524
2001 Jang Y, Chen H, Han J. Flow and Heat Transfer in a Rotating Square Channel With 45 deg Angled Ribs by Reynolds Stress Turbulence Model Journal of Turbomachinery-Transactions of the Asme. 123: 124-132. DOI: 10.1115/1.1333092  0.542
2000 Azad GS, Huang Y, Han J. Impingement heat transfer on dimpled surfaces using a transient liquid crystal technique Journal of Thermophysics and Heat Transfer. 14: 186-193. DOI: 10.2514/2.6530  0.783
2000 Chen H, Jang Y, Han J. Near-Wall Second-Moment Closure for Rotating Multiple-Pass Cooling Channels Journal of Thermophysics and Heat Transfer. 14: 201-209. DOI: 10.2514/2.6509  0.511
2000 Teng S, Sohn DK, Han JC. Unsteady wake effect on film temperature and effectiveness distributions for a gas turbine blade Journal of Turbomachinery. 122: 340-347. DOI: 10.1115/1.555457  0.519
2000 Azad GS, Han J, Boyle RJ. Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade Journal of Turbomachinery-Transactions of the Asme. 122: 725-732. DOI: 10.1115/1.1311284  0.793
2000 Azad GS, Han JC, Teng S, Boyle RJ. Heat transfer and pressure distributions on a gas turbine blade tip Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/1.1308567  0.793
2000 Chen H, Jang Y, Han J. Computation of heat transfer in rotating two-pass square channels by a second-moment closure model International Journal of Heat and Mass Transfer. 43: 1603-1616. DOI: 10.1016/S0017-9310(99)00227-6  0.511
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