Items where Author is "Sundaram, S"

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Venkatakrishnan, L and Sundaram, S and Viswanath, PR (2006) Hysteresis and broad flow features on a Swept Wing at high lift. Journal of Aircraft, 43 (4). pp. 1036-1043. ISSN 001-8669

Sundaram, S (2001) Investigation of Hysteresis Effects on a Swept Wing/Flap Configuration at High-Lift. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kumar, Rajeev and Sundaram, S (2000) Refurbishment and calibration studies of 0.3m water tunnel facility13; 13;. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sundaram, S (2000) Survey of Experimental Investigations on Lift Enhancement Using Gurney Flaps. Technical Report. National Aerospace Laboratories, Bangalore, India.

Subaschandar, N and Rajeev Kumar, - and Sundaram, S (1999) Drag Reduction Due to Riblets on a GAW(2) Airfoil. Journal of Aircraft, 36 (5). pp. 890-892.

Sundaram, S and Vishwanath, PR and Subhaschandar, N (1999) Viscous drag reduction using riblets on a swept wing. AIAA Journal, 37 (7). pp. 851-856. ISSN 0001-1452

Sundaram, S and Viswanath, PR and Subaschandra, N (1998) Studies on Drag Reduction Using Riblets on a Infinite Swept Wing. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sundaram, S and Grosche, FR and Kreplin, HP (1997) Cross-correlation measurements in Naturally Occurring Tollmien-Schlichting Waves. Technical Report. National Aeronautics and Space Administration.

Sundaram, S and Viswanath, PR and Rudrakumar, S (1996) Viscous drag reduction using riblets on NACA 0012 airfoil to moderate incidence. AIAA Journal, 34 (4). pp. 676-682.

Subaschandar, N and Rajeev, Kumar and Sundaram, S (1995) Drag Reduction Due to Riblets on a NACA 0012 Airfoil at Higher Angles of attack. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sundaram, S and Viswanath, PR and Rudrakumar, S (1994) Studies of turbulent. Drag reduction using riblets on a NACA 0012 aerofoil. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sundaram, S and Viswanath, PR (1992) Study on turbulent drag reduction using riblets on a flat plate. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaram, S and Yajnik, KS (1992) Experimental study on the evolution of a wall layer from a wake. AIAA Journal, 30 (12). pp. 2845-2851.

Sundaram, S and Yajnik, KS (1990) Experiments on the turbulent boundary layer on a flat plate in the wake of another flat plate. Technical Report. Experimental Aerodynamics Division, Bangalore, India.

Sundaram, S and Yajnik, KS (1990) The evolution of turbulent wall layer from free shear layer 13; 13;. In: 12th Symposium on Turbulence, 24-26 Sept 1990, United States.

Sundaram, S (1989) Calibration of vane anemometer. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaram, S (1988) Skin friction measurements in a turbulent boundary layer. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, PR and Sundaram, S and Madhavan, KT and Siddalingappa, SR and Yajnik, KS (1988) Flow visualisation of leading edge vortices on a Delta Wing by laser sheet technique. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS and Sundaram, S and Sivaram, R (1988) Evaluation of drag reduction by turbulence control devices 13; 13;. In: IUTAM Symposium on turbulence management and relaminarisation, 13-23 Jan 1987, Bangalore, India.

Sundaram, S (1987) Observations on the hydrodynamic flow visualisation at O.N.E.R.A. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS and Sundaram, S and Acharya, M (1983) Observations on large scale motions in highly disturbed boundary Layers. In: Structure of complex turbulent shear flow; Proceedings of the, 31 Aug - 03 Sept 1983, France.

Venkatakrishnan, L and Sundaram, S and Viswanath, PR Observations of hysteresis and broad flow features on a swept wing at high-lift. Project Report. National Aerospace Laboratories, Bangalore.

This list was generated on Thu Apr 17 06:24:49 2014 IST.