Three dimensional shock wave boundary layer interactions

1. Vemula, J. B. and Sinha, K., "Reynolds stress models applied to canonical shock-turbulence interaction", Journal of Turbulence, Volume 19, Issue 7, pp. 653-687, April 2017.

2. Vemula, J. B., Pathak, U. and Sinha, K., "Comparative Analysis Of Ramp-type And Busemann Intakes For Hypersonic Air-breathing Engine" Proceedings of 1st National Aerospace Propulsion Conference NAPC-2017, IIT Kanpur, March 15-17, 2017..

3. Vemula, J. B., Raje, P., Singh, R., Roy, S. and Sinha K., 10-11 August 2016, "Parametric study of the performance of two-dimensional Scramjet Intake", 18th Annual AeSI CFD Symposium, CSIR-National Aerospace Laboratories, Bangalore, India..

4. Vemula, J. B. and Sinha, K., "Reynolds Stress Models Applied to Shock-Turbulence Interaction" Ninth International Symposium on Turbulence and Shear Flow Phenomena TSFP-9, Melbourne, Australia, June 30-July 3, 2015..

PhD, Department of Aerospace Engineering, IIT Bombay, 2014-present

M.E, Department of Space Engineering and Rocketry (specialized in aerodynamics) from Birla Institute of technology, 2009-2011

B.Tech, Department of Aeronautical Engineering from Institute of Aeronautical Engineering (JNTU, HYD), 2005-2009

Project Assistant, Department of Aerospace Engineering, IISc, Bangalore CFD Engineer, Directorate of Aerodynamics, DRDL, Hyderabad.

V Jagadish Babu, P. Kumar, S. Das and J. K. Prasad,"Effect of Notched Cowl on Flow Field Inside a Super sonic Air-Intake" Department of Space Engineering and Rocketry Birla Institute of Technology, Mesra, Ranchi.

V Jagadish Babu, P. Kumar, S. Das and J. K. Prasad, "Studies of Supersonic Intake With Notched Cowl", XXVI National Convention Of Aerospace Engineers, 24-25 Nov, 2012.