Items where Author is "Khan, AA"
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Number of items: 10.
Conference or Workshop Item
Sathiyamoorthy, K and Jayaprakash, C and Khan, AA and Venkat Iyengar, S and Srinivas, J and Prateesh Kumar, P and Manjunath, P (2013) Development of Mach 3.6 water cooled Facility Nozzle. In: National Propulsion Conference 2013, 21 Feb 2013, Indian Institute of Madras, Chennai.
Jayaprakash, C and Sathiyamoorthy, K and Khan, AA and Venu, G and Venkat Iyengar, S and Srinivas, J and Prateesh Kumar, P and Manjunath, P (2013) Development of Mach 3.6 water cooled facility nozzle. In: National Propulsion Conference, Feb 2013 , Chennai.
Rahul, BV and Swapneel, Roy and Thanusha, MT and Khan, AA (2012) Unsteady Computation of over-Expanded flow in a convergent divergent nozzle. In: International Conference on Computing, Communications, Systems and Aeronautics, ICCCSA-2012, Hyderabad.
Khan, AA and Venkat Iyengar, S (2009) Numerical simulation of supersonic combustion of hydrogen in a vitiated air stream. In: 11th AeSI Annual CFD Symposium, 11-12 Aug 2009, Inidian Institute of Science, Bangalore, India.
Khan, AA and Shembharkar, TR (2008) Numerical Simulation of Supersonic Combustion in a Slant Cavity. In: 10th Annual CFD Symposium, 11-12 Aug 2008, NAL, Bangalore, India.
Khan, AA and Shembharkar, TR (2008) Viscous flow analysis in a convergent-divergent nozzle. In: Proceedings of the International Conference on Aerospace Science and Technology, 26-28 Jun 2008, Bangalore, India.
Khan, AA and Shembharkar, TR (2004) Computation of High Speed Cold Cavity Flow with a Commercial CFD Code. In: 31st National Conference on Fluid Mechanics & Fluid Power, 16-18 Dec 2004, Jadavpur University, Kolkata, India.
Roy, Swapneel and Thanusha, MT and Rahul, BV and Khan, AA (2013) Effect of Shocks on Mixing and Thrust in Over-expanded Nozzles. Frontiers in Aerospace Engineering, 2 (2). pp. 136-142. ISSN 2325-6796
Balaji, Sankar and Thennavarajan, S and Vijayendranath, V and Brijeshkumar , Shah and Khan, AA and Jana, S and Ramamurthy, S (2013) Aero-Thermodynamic modeling and gas path simulation for a twin spool turbo jet engine. Project Report. National Aerospace Laboratories, Bangalore.
Khan, AA and Vyas, VK and Muthu Selvan, G and Satish Kumar, M and Hariharan, R and Muralidhara, HS Design and erection of exhaust system for small gas turbine engine test facility. Project Report. National Aerospace Laboratories, Bangalore.