Ananthanarayanan Veeraragavan, Ph.D.
Affiliations: | 2009 | Aerospace Engineering | University of Maryland, College Park, College Park, MD |
Area:
combustion , laser diagnostics, compact power systems, and fuel cells.Google:
"Ananthanarayanan Veeraragavan"Parents
Sign in to add mentorChristopher P. Cadou | grad student | 2009 | University of Maryland | |
(Understanding the role of heat recirculation in enhancing the speed of premixed laminar flames in a parallel plate micro-combustor.) |
BETA: Related publications
See more...
Publications
You can help our author matching system! If you notice any publications incorrectly attributed to this author, please sign in and mark matches as correct or incorrect. |
Vanyai T, Grieve S, Street O, et al. (2020) Correction: Fundamental Scramjet Combustion Experiments Using Hydrocarbon Fuel Journal of Propulsion and Power. 0-0 |
Chang EWK, Chan WYK, Hopkins KJ, et al. (2020) Electrically-heated flat plate testing in a free-piston driven shock tunnel Aerospace Science and Technology. 103: 105856 |
Trudgian MA, Landsberg WO, Veeraragavan A. (2020) Experimental investigation of inclining the upstream wall of a scramjet cavity Aerospace Science and Technology. 99: 105767 |
Vanyai T, Grieve S, Street O, et al. (2019) Fundamental Scramjet Combustion Experiments Using Hydrocarbon Fuel Journal of Propulsion and Power. 35: 953-963 |
Wang J, Guan Z, Gurgenci H, et al. (2019) A computationally derived heat transfer correlation for in-tube cooling turbulent supercritical CO2 International Journal of Thermal Sciences. 138: 190-205 |
Duniam S, Veeraragavan A. (2019) Off-design performance of the supercritical carbon dioxide recompression Brayton cycle with NDDCT cooling for concentrating solar power Energy. 187: 115992 |
Landsberg WO, Veeraragavan A. (2019) Inclining and aerodynamically contouring a scramjet cavity's upstream wall Aerospace Science and Technology. 95: 105490 |
Wang J, Li J, Gurgenci H, et al. (2019) Computational investigations on convective flow and heat transfer of turbulent supercritical CO2 cooled in large inclined tubes Applied Thermal Engineering. 159: 113922 |
Landsberg WO, Wheatley V, Smart MK, et al. (2018) Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet Aiaa Journal. 56: 3802-3807 |
Wang J, Guan Z, Gurgenci H, et al. (2018) Numerical study on cooling heat transfer of turbulent supercritical CO2 in large horizontal tubes International Journal of Heat and Mass Transfer. 126: 1002-1019 |