Year |
Citation |
Score |
2020 |
Sahin I, Chen AF, Shiau C, Han J, Krewinkel R. Effect of 45-deg Rib Orientations on Heat Transfer in a Rotating Two-Pass Channel With Aspect Ratio from 4:1 to 2:1 Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4046492 |
0.551 |
|
2020 |
Shiau C, Sahin I, Ullah I, Han J, Mirzamoghadam AV, Riahi A, Stimpson C. Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4045990 |
0.44 |
|
2020 |
Nuntakulamarat M, Shiau C, Han J. Heat Transfer and Pressure Drop Measurements in a High Aspect Ratio Channel With Circular Pins and Strip Fins Journal of Thermal Science and Engineering Applications. 12. DOI: 10.1115/1.4045221 |
0.548 |
|
2020 |
Shiau C, Chen AF, Han J, Krewinkel R. Detailed Heat Transfer Coefficient Measurements on a Scaled Realistic Turbine Blade Internal Cooling System Journal of Thermal Science and Engineering Applications. 12. DOI: 10.1115/1.4044906 |
0.499 |
|
2019 |
Wright LM, Wang N, Zhang M, Alsaleem S, Han J. Turbine Blade Leading Edge Impingement Cooling From Normal Or Tangential Jets With Crossflow Effect Frontiers in Heat and Mass Transfer. 13. DOI: 10.5098/Hmt.13.9 |
0.43 |
|
2019 |
Wright LM, Yang S, Wu H, Han J, Lee C, Azad S, Um J. Heat Transfer in a Rotating, Blade-Shaped Serpentine Cooling Passage With Discrete Ribbed Walls at High Reynolds Numbers Journal of Heat Transfer. 142. DOI: 10.1115/1.4045243 |
0.602 |
|
2019 |
Chen AF, Shiau C, Han J, Krewinkel R. Heat Transfer in A Rotating Two-Pass Rectangular Channel Featuring A Converging Tip Turn With Various 45 Deg Rib Coverage Designs Journal of Thermal Science and Engineering Applications. 11: 1-42. DOI: 10.1115/1.4043471 |
0.513 |
|
2019 |
Wang N, Zhang M, Shiau C, Han J. Film Cooling Effectiveness From Two Rows of Compound Angled Cylindrical Holes Using Pressure-Sensitive Paint Technique Journal of Heat Transfer-Transactions of the Asme. 141: 42202. DOI: 10.1115/1.4042777 |
0.437 |
|
2019 |
Chen AF, Shiau C, Han J, Krewinkel R. Heat Transfer in a Rotating Two-Pass Rectangular Channel Featuring Reduced Cross-Sectional Area After Tip Turn (Aspect Ratio = 4:1 to 2:1) With Profiled 60 deg Angled Ribs Journal of Turbomachinery-Transactions of the Asme. 141: 71008. DOI: 10.1115/1.4042653 |
0.504 |
|
2019 |
Wang N, Han J. Swirl Impinging Cooling on an Airfoil Leading Edge Model at Large Reynolds Number Journal of Thermal Science and Engineering Applications. 11: 31006. DOI: 10.1115/1.4042151 |
0.406 |
|
2019 |
Shiau C, Sahin I, Wang N, Han J, Xu H, Fox M. Turbine Vane Endwall Film Cooling Comparison From Five Film-Hole Design Patterns And Three Upstream Injection Angles Journal of Thermal Science and Engineering Applications. 11: 31012. DOI: 10.1115/1.4042057 |
0.428 |
|
2019 |
Zhang M, Wang N, Han J. Overall effectiveness of film-cooled leading edge model with normal and tangential impinging jets International Journal of Heat and Mass Transfer. 139: 577-587. DOI: 10.1016/J.Ijheatmasstransfer.2019.05.037 |
0.546 |
|
2019 |
Zhang M, Wang N, Han J. Internal heat transfer of film-cooled leading edge model with normal and tangential impinging jets International Journal of Heat and Mass Transfer. 139: 193-204. DOI: 10.1016/J.Ijheatmasstransfer.2019.04.140 |
0.602 |
|
2019 |
Ullah I, Shiau C, Han J. Flat Plate Film Cooling with Linear and Curved Round-to-Diffusion Shaped Slots Using PSP Measurement Technique International Journal of Heat and Mass Transfer. 136: 755-766. DOI: 10.1016/J.Ijheatmasstransfer.2019.02.065 |
0.407 |
|
2019 |
Wang N, Shiau C, Han J, Xu H, Fox M. Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection International Journal of Heat and Mass Transfer. 133: 247-255. DOI: 10.1016/J.Ijheatmasstransfer.2018.12.079 |
0.527 |
|
2018 |
Shiau C, Chowdhury NHK, Han J, Mirzamoghadam AV, Riahi A. Transonic Turbine-Vane Film Cooling with Showerhead Effect Using Pressure-Sensitive Paint Measurement Technique Journal of Thermophysics and Heat Transfer. 32: 637-647. DOI: 10.2514/1.T5230 |
0.471 |
|
2018 |
Chen AF, Wu H, Wang N, Han J. Heat Transfer in a Rotating Cooling Channel (AR = 2:1) With Rib Turbulators and a Tip Turning Vane Journal of Heat Transfer. 140. DOI: 10.1115/1.4040260 |
0.609 |
|
2018 |
Zhang M, Wang N, Chen AF, Han J. Influence of turbine blade leading edge profile on film cooling with shaped holes Journal of Thermal Science and Engineering Applications. 10: 51006. DOI: 10.1115/1.4039703 |
0.462 |
|
2018 |
Wang N, Chen AF, Zhang M, Han J. Turbine Blade Leading Edge Cooling With One Row of Normal or Tangential Impinging Jets Journal of Heat Transfer-Transactions of the Asme. 140: 62201. DOI: 10.1115/1.4038691 |
0.427 |
|
2018 |
Shiau C, Chen AF, Han J, Azad S, Lee C. Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using Pressure-Sensitive Paint Technique Journal of Turbomachinery-Transactions of the Asme. 140: 21009. DOI: 10.1115/1.4038278 |
0.434 |
|
2018 |
Chen AF, Shiau C, Han J. Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions Journal of Turbomachinery-Transactions of the Asme. 140: 11006. DOI: 10.1115/1.4038150 |
0.457 |
|
2018 |
Chu H, Chen H, Han J. Numerical Simulation of Flow and Heat Transfer in Rotating Cooling Passage With Turning Vane in Hub Region Journal of Heat Transfer-Transactions of the Asme. 140: 21701. DOI: 10.1115/1.4037498 |
0.513 |
|
2017 |
Ekkad SV, Han J. A Transient Liquid Crystal Image Technique For Local Heat Transfer Distributions Near A Sharp 180° Turn Of A Two-Pass Smooth Square Channel Journal of Flow Visualization and Image Processing. 24: 127-139. DOI: 10.1615/Jflowvisimageproc.V24.I1-4.90 |
0.454 |
|
2017 |
Han J, Huang JJ, Lee C. Heat Transfer In Square Channels With Wedge-Shaped And Delta-Shaped Turbulence Promoters Journal of Enhanced Heat Transfer. 24: 101-116. DOI: 10.1615/Jenhheattransf.V24.I1-6.60 |
0.525 |
|
2017 |
Zhang YM, Han J, Lee C. Turbulent Flow In Circular Tubes With Twisted-Tape Inserts And Axial Interrupted Ribs Journal of Enhanced Heat Transfer. 24: 243-254. DOI: 10.1615/Jenhheattransf.V24.I1-6.170 |
0.392 |
|
2017 |
Wu H, Zirakzadeh H, Han J, Zhang L, Moon H. Heat Transfer in a Rib and Pin Roughened Rotating Multipass Channel With Hub Turning Vane and Trailing-Edge Slot Ejection Journal of Thermal Science and Engineering Applications. 10. DOI: 10.1115/1.4037584 |
0.605 |
|
2017 |
Chowdhury NHK, Zirakzadeh H, Han J. A Predictive Model for Preliminary Gas Turbine Blade Cooling Analysis Journal of Turbomachinery-Transactions of the Asme. 139: 91010. DOI: 10.1115/1.4036302 |
0.311 |
|
2017 |
Chowdhury NHK, Shiau C, Han J, Zhang L, Moon HK. Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration Journal of Turbomachinery-Transactions of the Asme. 139: 61003. DOI: 10.1115/1.4035162 |
0.457 |
|
2017 |
Chen AF, Shiau C, Han J. Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions Journal of Turbomachinery-Transactions of the Asme. 139: 31012. DOI: 10.1115/1.4034985 |
0.441 |
|
2017 |
Bashir MH, Shiau C, Han J. Film cooling effectiveness for three-row compound angle hole design on flat plate using PSP technique International Journal of Heat and Mass Transfer. 115: 918-929. DOI: 10.1016/J.Ijheatmasstransfer.2017.08.077 |
0.442 |
|
2017 |
Chowdhury NHK, Qureshi SA, Zhang M, Han J. Influence of turbine blade leading edge shape on film cooling with cylindrical holes International Journal of Heat and Mass Transfer. 115: 895-908. DOI: 10.1016/J.Ijheatmasstransfer.2017.08.020 |
0.48 |
|
2017 |
Yang S, Wu H, Han J, Zhang L, Moon H. Heat transfer in a smooth rotating multi-passage channel with hub turning vane and trailing-edge slot ejection International Journal of Heat and Mass Transfer. 109: 1-15. DOI: 10.1016/J.Ijheatmasstransfer.2017.01.059 |
0.503 |
|
2016 |
Li S, Yang S, Han J, Zhang L, Moon H. Turbine Blade Surface Phantom Cooling from Upstream Nozzle Trailing-Edge Ejection Journal of Thermophysics and Heat Transfer. 30: 770-781. DOI: 10.2514/1.T4796 |
0.483 |
|
2016 |
Li SJ, Lee J, Han JC, Zhang L, Moon HK. Turbine platform cooling and blade suction surface phantom cooling from simulated swirl purge flow Journal of Turbomachinery. 138. DOI: 10.1115/1.4032676 |
0.511 |
|
2016 |
Shiau CC, Chen AF, Han JC, Azad S, Lee CP. Full-scale turbine vane endwall film-cooling effectiveness distribution using pressure-sensitive paint technique Journal of Turbomachinery. 138. DOI: 10.1115/1.4032166 |
0.548 |
|
2016 |
Li S, Lee J, Han J, Zhang L, Moon H. Influence of mainstream turbulence on turbine blade platform cooling from simulated swirl purge flow Applied Thermal Engineering. 101: 678-685. DOI: 10.1016/J.Applthermaleng.2016.01.056 |
0.486 |
|
2015 |
Chen AF, Li S, Han J. Film Cooling for Cylindrical and Fan-Shaped Holes Using Pressure-Sensitive Paint Measurement Technique Journal of Thermophysics and Heat Transfer. 29: 775-784. DOI: 10.2514/1.T4518 |
0.491 |
|
2015 |
Yang S, Han J, Azad S, Lee C. Heat Transfer in Rotating Serpentine Coolant Passage With Ribbed Walls at Low Mach Numbers Journal of Thermal Science and Engineering Applications. 7: 11013. DOI: 10.1115/1.4028905 |
0.579 |
|
2015 |
Rezasoltani M, Lu K, Schobeiri MT, Han J. A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness Under Rotation Condition Journal of Turbomachinery-Transactions of the Asme. 137: 51009. DOI: 10.1115/1.4028745 |
0.522 |
|
2014 |
Lei J, Li S, Han J, Zhang L, Moon H. Effect of a Turning Vane on Heat Transfer in Rotating Multipass Rectangular Smooth Channel Journal of Thermophysics and Heat Transfer. 28: 417-427. DOI: 10.2514/1.T4311 |
0.563 |
|
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 |
0.712 |
|
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 |
0.839 |
|
2014 |
Liu K, Yang S, Han J. Influence of Coolant Density on Turbine Platform Film-Cooling With Stator–Rotor Purge Flow and Compound-Angle Holes Journal of Thermal Science and Engineering Applications. 6: 41007. DOI: 10.1115/1.4026964 |
0.45 |
|
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 |
0.842 |
|
2014 |
Liu K, Yang S, Han J. Influence of Coolant Density on Turbine Blade Film-Cooling With Axial and Compound Shaped Holes Journal of Heat Transfer-Transactions of the Asme. 136: 44501. DOI: 10.1115/1.4025901 |
0.526 |
|
2014 |
Li S, Yang S, Han J. Effect of Coolant Density on Leading Edge Showerhead Film Cooling Using the Pressure Sensitive Paint Measurement Technique Journal of Turbomachinery-Transactions of the Asme. 136: 51011. DOI: 10.1115/1.4025225 |
0.428 |
|
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 |
0.821 |
|
2013 |
Han J. Fundamental Gas Turbine Heat Transfer Journal of Thermal Science and Engineering Applications. 5: 21007. DOI: 10.1115/1.4023826 |
0.471 |
|
2013 |
Lei J, Li S, Han J, Zhang L, Moon H. Heat Transfer in Rotating Multipass Rectangular Ribbed Channel With and Without a Turning Vane Journal of Heat Transfer-Transactions of the Asme. 135: 41903. DOI: 10.1115/1.4023040 |
0.572 |
|
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 |
0.835 |
|
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 |
0.8 |
|
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 |
0.772 |
|
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 |
0.835 |
|
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 |
0.806 |
|
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 |
0.786 |
|
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 |
0.84 |
|
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 |
0.845 |
|
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 |
0.778 |
|
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 |
0.794 |
|
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 |
0.804 |
|
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 |
0.839 |
|
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 |
0.847 |
|
2010 |
Han J, Huh M. Recent Studies in Turbine Blade Internal Cooling Heat Transfer Research. 41: 803-828. DOI: 10.1615/Heattransres.V41.I8.30 |
0.393 |
|
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 |
0.656 |
|
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 |
0.837 |
|
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 |
0.83 |
|
2009 |
Gao Z, Han J. Influence of Film-Hole Shape and Angle on Showerhead Film Cooling Using PSP Technique Journal of Heat Transfer-Transactions of the Asme. 131: 61701. DOI: 10.1115/1.3082413 |
0.483 |
|
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 |
0.791 |
|
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 |
0.839 |
|
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 |
0.704 |
|
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 |
0.805 |
|
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 |
0.834 |
|
2008 |
Yang H, Chen HC, Han JC, Moon HK. Film-cooling prediction on rotor blade leading edge in 1-1/2 turbine stage Journal of Thermophysics and Heat Transfer. 22: 201-209. DOI: 10.2514/1.30624 |
0.583 |
|
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 |
0.772 |
|
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 |
0.697 |
|
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 |
0.835 |
|
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 |
0.683 |
|
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 |
0.838 |
|
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 |
0.805 |
|
2008 |
Yang H, Chen HC, Han JC, Moon HK. Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage International Journal of Heat and Mass Transfer. 51: 3066-3081. DOI: 10.1016/J.Ijheatmasstransfer.2007.09.025 |
0.563 |
|
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 |
0.716 |
|
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 |
0.801 |
|
2007 |
Su G, Chen H, Han J. Computation of Flow and Heat Transfer in Rotating Rectangular Channels (AR=4:1) With Pin-Fins by a Reynolds Stress Turbulence Model Journal of Heat Transfer-Transactions of the Asme. 129: 685-696. DOI: 10.1115/1.2717935 |
0.584 |
|
2007 |
Ahn J, Schobeiri MT, Han JC, Moon HK. Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes International Journal of Heat and Mass Transfer. 50: 15-25. DOI: 10.1016/J.Ijheatmasstransfer.2006.06.028 |
0.53 |
|
2006 |
Han J, Dutta S. Recent developments in turbine blade internal cooling. Annals of the New York Academy of Sciences. 934: 162-178. PMID 11460626 DOI: 10.1111/J.1749-6632.2001.Tb05850.X |
0.465 |
|
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 |
0.789 |
|
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 |
0.815 |
|
2006 |
Yang H, Chen H, Han J. Film-Cooling Prediction on Turbine Blade Tip with Various Film Hole Configurations Journal of Thermophysics and Heat Transfer. 20: 558-568. DOI: 10.2514/1.18422 |
0.559 |
|
2006 |
Han J. Turbine Blade Cooling Studies at Texas A&M University: 1980-2004 Journal of Thermophysics and Heat Transfer. 20: 161-187. DOI: 10.2514/1.15403 |
0.555 |
|
2006 |
Yang H, Chen H, Han J. Turbine Rotor with Various Tip Configurations Flow and Heat Transfer Prediction Journal of Thermophysics and Heat Transfer. 20: 80-91. DOI: 10.2514/1.14949 |
0.566 |
|
2006 |
Han J, Chen H. Turbine Blade Internal Cooling Passages with Rib Turbulators Journal of Propulsion and Power. 22: 226-248. DOI: 10.2514/1.12793 |
0.566 |
|
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 |
0.771 |
|
2006 |
Ahn J, Schobeiri MT, Han JC, Moon HK. Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint Journal of Heat Transfer. 128: 879-888. DOI: 10.1115/1.2241945 |
0.535 |
|
2006 |
Han JC. Turbine blade cooling studies at Texas A&M University: 1980-2004 Journal of Thermophysics and Heat Transfer. 20: 161-187. |
0.442 |
|
2005 |
Lee E, Wright LM, Han J. Heat Transfer in Rotating Rectangular Channels with V-Shaped and Angled Ribs Journal of Thermophysics and Heat Transfer. 19: 48-56. DOI: 10.2514/1.9065 |
0.549 |
|
2005 |
Parsons JA, Han J. Jet-impingement heat transfer in rotating channels with staggered extraction flow Journal of Thermophysics and Heat Transfer. 19: 156-162. DOI: 10.2514/1.8268 |
0.521 |
|
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 |
0.834 |
|
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 |
0.807 |
|
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 |
0.788 |
|
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 |
0.753 |
|
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 |
0.805 |
|
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 |
0.716 |
|
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 |
0.679 |
|
2004 |
Han J. Recent Studies in Turbine Blade Cooling International Journal of Rotating Machinery. 10: 443-457. DOI: 10.1155/S1023621X04000442 |
0.595 |
|
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 |
0.797 |
|
2004 |
Kwak JS, Ahn J, Han J. Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade International Journal of Heat and Mass Transfer. 47: 5651-5663. DOI: 10.1016/J.Ijheatmasstransfer.2004.07.029 |
0.557 |
|
2004 |
Su G, Chen H, Han J, Heidmann JD. Computation of flow and heat transfer in rotating two-pass rectangular channels (AR = 1:1, 1:2, and 1:4) with smooth walls by a Reynolds stress turbulence model International Journal of Heat and Mass Transfer. 47: 5665-5683. DOI: 10.1016/J.Ijheatmasstransfer.2004.07.019 |
0.558 |
|
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 |
0.726 |
|
2003 |
Kwak JS, Ahn J, Han J, Lee CP, Bunker RS, Boyle R, Gaugler R. Heat Transfer Coefficients on the Squealer Tip and Near-Tip Regions of a Gas Turbine Blade With Single or Double Squealer Journal of Turbomachinery-Transactions of the Asme. 125: 778-787. DOI: 10.1115/1.1626684 |
0.572 |
|
2003 |
Kwak JS, Han J. Heat Transfer Coefficients and Film Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade Journal of Turbomachinery-Transactions of the Asme. 125: 648-657. DOI: 10.1115/1.1622712 |
0.63 |
|
2003 |
Griffith TS, Al-Hadhrami L, Han J. Heat Transfer in Rotating Rectangular Cooling Channels (AR=4) With Dimples Journal of Turbomachinery-Transactions of the Asme. 125: 555-563. DOI: 10.1115/1.1571850 |
0.555 |
|
2003 |
Kwak JS, Han J. Heat transfer coefficients on the squealer tip and near squealer tip regions of a gas turbine blade Journal of Heat Transfer-Transactions of the Asme. 125: 669-677. DOI: 10.1115/1.1571849 |
0.563 |
|
2003 |
Kwak JS, Han J. Heat Transfer Coefficients and Film-Cooling Effectiveness on a Gas Turbine Blade Tip Journal of Heat Transfer-Transactions of the Asme. 125: 494-502. DOI: 10.1115/1.1565096 |
0.622 |
|
2003 |
AL-Hadhrami L, Griffith T, Han J. Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=2) With Five Different Orientations of 45 Deg V-Shaped Rib Turbulators Journal of Heat Transfer-Transactions of the Asme. 125: 232-242. DOI: 10.1115/1.1561455 |
0.558 |
|
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 |
0.837 |
|
2003 |
Al-Hadhrami L, Han J. Effect of rotation on heat transfer in two-pass square channels with five different orientations of 45° angled rib turbulators International Journal of Heat and Mass Transfer. 46: 653-669. DOI: 10.1016/S0017-9310(02)00325-3 |
0.551 |
|
2002 |
Kwak JS, Han J. Heat-Transfer Coefficients of a Turbine Blade-Tip and Near-Tip Regions Journal of Thermophysics and Heat Transfer. 17: 297-303. DOI: 10.2514/2.6776 |
0.566 |
|
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 |
0.827 |
|
2002 |
Griffith TS, Al-Hadhrami L, Han J. Heat Transfer in Rotating Rectangular Cooling Channels (AR=4) With Angled Ribs Journal of Heat Transfer-Transactions of the Asme. 124: 617-625. DOI: 10.1115/1.1471525 |
0.566 |
|
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 |
0.839 |
|
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 |
0.863 |
|
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 |
0.846 |
|
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 |
0.817 |
|
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 |
0.847 |
|
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 |
0.653 |
|
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 |
0.721 |
|
2001 |
Du H, Ekkad SV, Han J, Lee CP. Detailed Film Cooling Measurements over a Gas Turbine Blade Using a Transient Liquid Crystal Image Technique International Journal of Rotating Machinery. 7: 415-424. DOI: 10.1155/S1023621X01000367 |
0.558 |
|
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 |
0.711 |
|
2001 |
Parsons JA, Han J. Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels with Film Coolant Extraction International Journal of Rotating Machinery. 7: 87-103. DOI: 10.1155/S1023621X01000082 |
0.553 |
|
2001 |
Han J, Ekkad S. Recent Development in Turbine Blade Film Cooling International Journal of Rotating Machinery. 7: 21-40. DOI: 10.1155/S1023621X01000033 |
0.471 |
|
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 |
0.684 |
|
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 |
0.694 |
|
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 |
0.726 |
|
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 |
0.818 |
|
2000 |
Ekkad S, Huang Y, Han J. Impingement Heat Transfer Measurements Under an Array of Inclined Jets Journal of Thermophysics and Heat Transfer. 14: 286-288. DOI: 10.2514/2.6524 |
0.425 |
|
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 |
0.703 |
|
2000 |
Zhang YM, Azad GM, Han J, Lee C. Turbulent Heat Transfer Enhancement and Surface Heating Effect in Square Channels with Wavy, and Twisted Tape Inserts with Interrupted Ribs Journal of Enhanced Heat Transfer. 7: 35-49. DOI: 10.1615/Jenhheattransf.V7.I1.40 |
0.555 |
|
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 |
0.692 |
|
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 |
0.858 |
|
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 |
0.852 |
|
2000 |
Ekkad SV, Han J. A transient liquid crystal thermography technique for gas turbine heat transfer measurements Measurement Science and Technology. 11: 957-968. DOI: 10.1088/0957-0233/11/7/312 |
0.56 |
|
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 |
0.694 |
|
1999 |
Ekkad SV, Huang Y, Han J. Impingement Heat Transfer on a Target Plate with Film Cooling Holes Journal of Thermophysics and Heat Transfer. 13: 522-528. DOI: 10.2514/2.6471 |
0.524 |
|
1999 |
Akella KV, Han J. Impingement Cooling in Rotating Two-Pass Rectangular Channels with Ribbed Walls Journal of Thermophysics and Heat Transfer. 13: 364-371. DOI: 10.2514/2.6447 |
0.477 |
|
1999 |
Ekkad SV, Han J. Heat Transfer Distributions on a Cylinder with Simulated Thermal Barrier Coating Spallation Journal of Thermophysics and Heat Transfer. 13: 76-81. DOI: 10.2514/2.6403 |
0.527 |
|
1998 |
Akella KV, Han J. Impingement Cooling in Rotating Two-Pass Rectangular Channels Journal of Thermophysics and Heat Transfer. 12: 582-588. DOI: 10.2514/2.6379 |
0.458 |
|
1998 |
Chandra PR, Fontenot ML, Han J. Effect of Rib Profiles on Turbulent Channel Flow Heat Transfer Journal of Thermophysics and Heat Transfer. 12: 116-118. DOI: 10.2514/2.6312 |
0.587 |
|
1998 |
Huang Y, Ekkad SV, Han J. Detailed heat transfer distributions under an array of orthogonal impinging jets Journal of Thermophysics and Heat Transfer. 12: 73-79. DOI: 10.2514/2.6304 |
0.555 |
|
1998 |
Han J, Dutta S. Rotational Effects On The Turbine Blade Coolant Passage Heat Transfer Annual Review of Heat Transfer. 9: 269-314. DOI: 10.1615/Annualrevheattransfer.V9.70 |
0.55 |
|
1998 |
Mehendale AB, Jiang HW, Ekkad SV, Han J. Effect of Film Injection Location on Local Heat Transfer Coefficient on a Gas Turbine Blade International Journal of Rotating Machinery. 4: 163-174. DOI: 10.1155/S1023621X98000141 |
0.535 |
|
1998 |
Ekkad SV, Huang Y, Han J. Detailed heat transfer distributions in two-pass square channels with rib turbulators and bleed holes International Journal of Heat and Mass Transfer. 41: 3781-3791. DOI: 10.1016/S0017-9310(98)00099-4 |
0.557 |
|
1998 |
Parsons JA, Han J. Rotation effect on jet impingement heat transfer in smooth rectangular channels with heated target walls and radially outward cross flow International Journal of Heat and Mass Transfer. 41: 2059-2071. DOI: 10.1016/S0017-9310(97)00286-X |
0.551 |
|
1997 |
Dutta S, Andrews MJ, Han JC. Turbulent flow and heat transfer in rotating different aspect ratio channels Journal of Thermophysics and Heat Transfer. 11: 318-319. DOI: 10.2514/2.6244 |
0.456 |
|
1997 |
Zhang YM, Han J, Lee C. Heat Transfer and Friction Characteristics of Turbulent Flow in Circular Tubes with Twisted-Tape Inserts and Axial Interrupted Ribs Journal of Enhanced Heat Transfer. 4: 297-308. DOI: 10.1615/Jenhheattransf.V4.I4.50 |
0.538 |
|
1997 |
Ekkad SV, Zapata D, Han J. Film effectiveness over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method Journal of Turbomachinery-Transactions of the Asme. 119: 587-593. DOI: 10.1115/1.2841162 |
0.484 |
|
1997 |
Ekkad SV, Han J. Detailed heat transfer distributions in two-pass square channels with rib turbulators International Journal of Heat and Mass Transfer. 40: 2525-2537. DOI: 10.1016/S0017-9310(96)00318-3 |
0.535 |
|
1996 |
Ekkad SV, Han J. Heat Transfer Inside and Downstream of Cavities Using Transient Liquid Crystal Method Journal of Thermophysics and Heat Transfer. 10: 511-516. DOI: 10.2514/3.818 |
0.502 |
|
1996 |
Du H, Ekkad SV, Han J. Surface Heat Transfer Visualization On A Model Gas Turbine Blade Using A Transient Liquid Crystal Image Technique Journal of Flow Visualization and Image Processing. 3: 141-152. DOI: 10.1615/Jflowvisimageproc.V3.I2-3.30 |
0.421 |
|
1996 |
Ekkad SV, Du H, Han J. Local Heat Transfer Coefficient And Film Effectiveness Distributions On A Cylindrical Leading Edge Model Using A Transient Liquid Crystal Image Method Journal of Flow Visualization and Image Processing. 3: 129-140. DOI: 10.1615/Jflowvisimageproc.V3.I2-3.20 |
0.472 |
|
1996 |
Dutta S, Andrews MJ, Han JC. Prediction of turbulent heat transfer in rotating smooth square ducts International Journal of Heat and Mass Transfer. 39: 2505-2514. DOI: 10.1016/0017-9310(95)00319-3 |
0.537 |
|
1996 |
Dutta S, Han JC, Lee CP. Local heat transfer in a rotating two-pass ribbed triangular duct with two model orientations International Journal of Heat and Mass Transfer. 39: 707-715. DOI: 10.1016/0017-9310(95)00171-9 |
0.561 |
|
1995 |
Dutta S, Andrews MJ, Han JC. Simulation of turbulent heat transfer in a rotating duct Journal of Thermophysics and Heat Transfer. 9: 381-382. DOI: 10.2514/3.676 |
0.51 |
|
1995 |
Ekkad SV, Han J. Local Heat Transfer Distributions Near A Sharp 180° Turn Of A Two-Pass Smooth Square Channel Using A Transient Liquid Crystal Image Technique Journal of Flow Visualization and Image Processing. 2: 285-297. DOI: 10.1615/Jflowvisimageproc.V2.I3.80 |
0.454 |
|
1995 |
Parsons JA, Han J, Zhang Y. Effect of model orientation and wall heating condition on local heat transfer in a rotating two-pass square channel with rib turbulators International Journal of Heat and Mass Transfer. 38: 1151-1159. DOI: 10.1016/0017-9310(94)00246-R |
0.557 |
|
1994 |
Mehendale AB, Ekkad SV, Han J. Mainstream turbulence effect on film effectiveness and heat transfer coefficient of a gas turbine blade with air and CO2 film injection International Journal of Heat and Mass Transfer. 37: 2707-2714. DOI: 10.1016/0017-9310(94)90387-5 |
0.567 |
|
1993 |
Han J, Huang JJ, Lee C. Augmented Heat Transfer in Square Channels with Wedge-Shaped and Delta-Shaped Turbulence Promoters Journal of Enhanced Heat Transfer. 1: 37-52. DOI: 10.1615/Jenhheattransf.V1.I1.40 |
0.526 |
|
1988 |
Han JC. HEAT TRANSFER AND FRICTION CHARACTERISTICS IN RECTANGULAR CHANNELS WITH RIB TURBULATORS Journal of Heat Transfer. 110: 321-328. |
0.422 |
|
1984 |
Han JC. HEAT TRANSFER AND FRICTION IN CHANNELS WITH TWO OPPOSITE RIB-ROUGHENED WALLS Journal of Heat Transfer. 106: 774-781. |
0.466 |
|
1979 |
Han JT. HEAT TRANSFER IN A PARTIALLY-BLOCKED SODIUM-COOLED ROD BUNDLE Simulation. 187-191. |
0.404 |
|
1966 |
Han JT. Heat transfer in a partially-blocked sodium-cooled rod bundle . |
0.404 |
|
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