You are here

Publications 2013

  • R. J. Yentsch and D. V. Gaitonde, "Unsteady Three-Dimensional Phenomena in Mode-Transition Simulations of the HIFiRE-2 Scramjet Flowpath.", AIAA Paper 2013-3753, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, July 14-17, 2013, doi: 10.2514/6.2013-3753.

  • R. L. Speth and D. V. Gaitonde, "Parametric Study of a Mach 1.3 Cold Jet Excited by the Flapping Mode Using Plasma Actuators.", Computers and Fluids, 84:16-34, 2013, doi: 10.1016/j.compfluid.2013.04.028.

  • D. V. Gaitonde, "Analysis of plasma-based flow control mechanisms through large-eddy simulations.", Computers and Fluids, 85:19-26, 2013, doi: 10.1016/j.compfluid.2012.09.004.

  • N. Mullenix, D. V. Gaitonde, and M. R. Visbal, "Spatially Developing Supersonic Turbulent Boundary Layer with a Body-Force-Based Method.", AIAA Journal, 51:1805-1819, 2013, doi: 10.2514/1.J051861.

  • R. Yentsch and D. Gaitonde, "Numerical Investigation of the HIFiRE-2 Scramjet Flowpath.", AIAA Paper 2013-119, 2013, doi: 10.2514/6.2013-119.

  • N. Mullenix and D. Gaitonde, "Analysis of Unsteady Behavior in Shock/Turbulent Boundary Layer Interactions with Large-Eddy Simulations.", AIAA Paper 2013-404, 2013, doi: 10.2514/6.2013-404.

  • D. Gaitonde, K. Sahin, K. Shaler, B. Glaz, and S. Dinavahi, "High-Fidelity Simulations of NS-DBD-based Control of a Stalled NACA0015 Airfoiol.", AIAA Paper 2013-1118, 2013, doi: 10.2514/6.2013-1118.

  • N. Mullenix and D. Gaitonde, "Development of a Conjugate Heat Transfer Simulation Tool for Anisotropic Thermal Protection Systems.", AIAA Paper 2013-602, 2013, doi: 10.2514/6.2013-602.

  • M. Nishihara, D. Gaitonde, and I. V. Adamovich, "Effect of Nanosecond Pulse Discharges on Oblique Shock and Shcok Wave-Boundary Layer Interaction.", AIAA Paper 2013-0461, 2013, doi: 10.2514/6.2013-461.

  • D. V. Gaitonde, "Progress in Shock Wave/Boundary Layer Interactions.", AIAA Paper 2013-2607 (Invited Review Article), 2013, doi: 10.2514/6.2013-2607.

  • R. L. Speth and D. V. Gaitonde, "Correlation of Near Field Pressure With Coherent Structures In An Excited Mach 1.3 Jet.", ASME FEDSM2013-16495, Incline Village, NV, 2013, doi:10.1115/FEDSM2013-16495.