Shantanu Mhetras, Ph.D. - Publications

Affiliations: 
2006 Texas A & M University, College Station, TX, United States 
Area:
Mechanical Engineering

24 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
2015 Otto M, Hodges JD, Kapat JS, Mhetras S, Ricklick MA. Combination of ribs and pins for internal cooling 51st Aiaa/Sae/Asee Joint Propulsion Conference 0.315
2014 Narzary D, Liu K, Han JC, Mhetras S, Landis K. Turbine blade tip film-cooling and heat transfer measurements at high blowing ratios Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2014-25793  0.666
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  0.449
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  0.476
2012 Gao Z, Narzary DP, Mhetras S, Han JC. Upstream vortex effect on turbine platform film cooling with typical purge flow Journal of Thermophysics and Heat Transfer. 26: 75-84. DOI: 10.2514/1.42411  0.786
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  0.679
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  0.798
2009 Suryanarayanan A, Mhetras SP, Schobeiri MT, Han JC. Film-cooling effectiveness on a rotating blade platform Journal of Turbomachinery. 131. DOI: 10.1115/1.2752184  0.722
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  0.803
2008 Gao Z, Narzary D, Mhetras S, Han JC. Upstream vortex effects on turbine blade platform film cooling with typical stator-rotor purge flow Asme International Mechanical Engineering Congress and Exposition, Proceedings. 8: 707-718. DOI: 10.1115/IMECE2007-41717  0.766
2008 Mhetras S, Han JC, Rudolph R. Film-cooling effectiveness from shaped film cooling holes for a gas turbine blade Proceedings of the Asme Turbo Expo. 4: 837-848. DOI: 10.1115/GT2008-50916  0.689
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  0.643
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  0.801
2007 Narzary DP, Gao Z, Mhetras S, Han JC. Effect of unsteady wake on film-cooling effectiveness distribution on a gas turbine blade with compound shaped holes Proceedings of the Asme Turbo Expo. 4: 79-91. DOI: 10.1115/GT2007-27070  0.812
2007 Gao Z, Narzary DP, Mhetras S, Han JC. Full coverage film cooling for a turbine blade with axial shaped holes Collection of Technical Papers - 39th Aiaa Thermophysics Conference. 1: 180-193.  0.823
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  0.854
2006 Mhetras S, Han JC. Effect of superposition on spanwise film-cooling effectiveness distribution on a gas turbine blade American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. DOI: 10.1115/IMECE2006-15084  0.836
2006 Mhetras S, Narzary D, Gao Z, Han JC. Effect of a cutback squealer and cavity depth on film-cooling effectiveness for a gas turbine blade tip Collection of Technical Papers - 9th Aiaa/Asme Joint Thermophysics and Heat Transfer Conference Proceedings. 2: 1399-1413.  0.83
2006 Mhetras S, Yang H, Gao Z, Han JC. Film-cooling effectiveness on squealer cavity and rim walls of gas-turbine blade tip Journal of Propulsion and Power. 22: 889-899.  0.832
2006 Mhetras S, Han JC. Effect of unsteady wake on full coverage film-cooling effectiveness for a gas turbine blade Collection of Technical Papers - 9th Aiaa/Asme Joint Thermophysics and Heat Transfer Conference Proceedings. 2: 1382-1398.  0.854
2005 Mhetras S, Yang H, Gao Z, Han JC. Film-cooling effectiveness on squealer rim walls and squealer cavity floor of a gas turbine blade tip using pressure sensitive paint Proceedings of the Asme Turbo Expo. 3: 397-408. DOI: 10.1115/GT2005-68387  0.835
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  0.832
2004 Ahn J, Mhetras S, Han JC. Film-cooling effectiveness on a gas turbine blade tip using pressure sensitive paint Proceedings of the Asme Turbo Expo 2004. 3: 241-250.  0.796
2002 Mhetras S, Lau SC. Experiments on effect of jet impingement on heat transfer in annular channels with parallel and counter flows American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. 372: 39-48. DOI: 10.1115/IMECE2002-33658  0.359
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