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Aroon K. Viswanathan, Ph.D. - Publications

Affiliations: 
2006 Virginia Polytechnic Institute and State University, Blacksburg, VA, United States 
Area:
Mechanical Engineering
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17 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
2013 Tafti DK, Nagendra K, Viswanathan AK. Gas-Side Fouling Of Fin Surfaces In Exhaust Gas Recirculators Wit Transactions On State-of-the-Art in Science and Engineering. 63: 1-37. DOI: 10.2495/978-1-84564-818-3/01  0.455
2011 Nagendra K, Tafti DK, Viswanathan AK. Modeling of soot deposition in wavy-fin exhaust gas recirculator coolers International Journal of Heat and Mass Transfer. 54: 1671-1681. DOI: 10.1016/J.Ijheatmasstransfer.2010.10.033  0.556
2008 Viswanathan AK, Squires KD, Forsythe JR. Detached-eddy simulation around a forebody with rotary motion Aiaa Journal. 46: 2191-2201. DOI: 10.2514/1.4756  0.51
2007 Viswanathan AK, Tafti DK. Capturing effects of rotation in sudden expansion channels using detached eddy simulation Aiaa Journal. 45: 2100-2102. DOI: 10.2514/1.27429  0.679
2007 Viswanathan AK, Tafti DK. Investigation of detached eddy simulations in capturing the effects of coriolis forces and centrifugal buoyancy in ribbed ducts Journal of Heat Transfer. 129: 778-789. DOI: 10.1115/1.2717944  0.687
2006 Viswanathan AK, Tafti DK. Large eddy simulation of fully developed flow and heat transfer in a rotating duct with 45° ribs Proceedings of the Asme Turbo Expo. 3: 215-229. DOI: 10.1115/GT2006-90229  0.655
2006 Viswanathan AK, Tafti DK. A comparative study of des and URANS for flow prediction in a two-pass internal cooling duct Journal of Fluids Engineering, Transactions of the Asme. 128: 1336-1345. DOI: 10.1115/1.2353279  0.707
2006 Viswanathan AK, Tafti DK. Detached eddy simulation of flow and heat transfer in fully developed rotating internal cooling channel with normal ribs International Journal of Heat and Fluid Flow. 27: 351-370. DOI: 10.1016/J.Ijheatfluidflow.2005.12.003  0.748
2006 Viswanathan AK, Tafti DK. Detached eddy simulation of turbulent flow and heat transfer in a two-pass internal cooling duct International Journal of Heat and Fluid Flow. 27: 1-20. DOI: 10.1016/J.Ijheatfluidflow.2005.07.002  0.757
2005 Viswanathan AK, Tafti DK. A comparative study of DES and URANS in a two-pass internal cooling duct with normal ribs American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. 376: 35-50. DOI: 10.1115/IMECE2005-79288  0.739
2005 Viswanathan AK, Tafti DK. Detached eddy simulation of flow and heat transfer in a stationary internal cooling duct with skewed ribs Proceedings of the Asme Turbo Expo. 3: 191-206. DOI: 10.1115/GT2005-68118  0.736
2005 Viswanathan AK, Tafti DK. Large eddy simulation in a duct with rounded skewed ribs Proceedings of the Asme Turbo Expo. 3: 177-189. DOI: 10.1115/GT2005-68117  0.721
2005 Viswanathan AK, Tafti DK, Abdel-Wahab S. Large Eddy simulation of flow and heat transfer in an internal cooling duct with high blockage ratio 45° staggered ribs Proceedings of the Asme Turbo Expo. 3: 107-119. DOI: 10.1115/GT2005-68086  0.716
2004 Viswanathan AK, Tafti DK. Detached eddy simulation of turbulent flow and heat transfer in a ribbed duct Proceedings of the Asme Heat Transfer/Fluids Engineering Summer Conference 2004, Ht/Fed 2004. 2: 345-361. DOI: 10.1115/1.2033010  0.727
2004 Viswanathan AK, Tafti DK. Detached eddy simulation of turbulent flow and heat transfer in a ribbed duct Proceedings of the Asme Heat Transfer/Fluids Engineering Summer Conference 2004, Ht/Fed 2004. 2: 345-361.  0.631
2003 Viswanathan AK, Squires KD, Forsythe JR. Detached Eddy Simulation of the flow over an axisymmetric cavity 41st Aerospace Sciences Meeting and Exhibit.  0.5
2003 Viswanathan AK, Klismith KR, Forsythe JR, Squire KD. Detached-Eddy Simulation around a forebody at high angle of attack 41st Aerospace Sciences Meeting and Exhibit.  0.469
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