2.7 Performance of Actual Nozzles.
1, January-February 2010,.
Sirinivasa Rao - Co-flow jets.
3.2 Equations of Motion for a Normal Shock Wave.3 Normal Shock Waves.11.16 Internal Shock Attachment.5.4 Linearization of the Potential Equation.The following projects are in progress/completed at the HSA lab in IIT Kanpur -.Vinoth.R and Rathakrishnan E em Effect of impinging plate geometry on the self-excitation of subsonic impinging jets, Journal of Fluids and Structures Vol.2, February 2010,.G Balu - Experimental Investigation of Isolator Performance, Scientist F, drdl, Hyderabad, India.International Review of Mechanical Engineering (ireme).1, Februrary 2009, pp 29-38.Elangovan and Rathakrishnan E, em Perforated Arc-Tabs for Jet Control, Journal of Turbo and Jet Engines, Vol.Office, high Speed Aerodynamics Laboratory, department plugin manager 2.1 crack of Aerospace Engineering, indian Institute of Technology, Kanpur.Keynote Lecutre on "Innovative Tabs for Supersonic Jet Control" at ASV 11 Conference, June 2-5, 2011, Niigata, norton 360 v 5.0 keygen Japan.Professor Rathakrishnan has introduced and developed the following Graduate level courses at IIT Kanpur -.10.12 Instrumentation and Calibration of Wind Tunnels.Dhananjeya Rao, Swaminathan S and Rathakrishnan E, Interaction of supersonic jet across supersonic flow over a sharp cone aiaa, 25th aiaa Applied Aerodynamics Conference, 25-28, June 2007, Miami, Florida.1.18 Compressible Flow Regimes.5.3 General Potential Equation for Three-Dimensional Flow.The acoustic investigations clearly brought out the ovarall acoustic load and its directional senstivity as a function of the nozzle pressure ratio, inter-nozzle spacing and number of surrounding jets and their configuration.Shashank Khurana, Kojiro Suzuki and Ethirajan Rathakrishnan em Flow Field around a Blunted-nosed Body with Spike, Int.11.10 External Supersonic Compression.
4.6 Weak Oblique Shocks.