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Madhavan, KT and Sajeer, Ahmed and Suriyanarayanan, P and Ramesh, G CALIBRATION OF 0.55m LOW SPEED WIND TUNNEL FOR LOW REYNOLDS NUMBER STUDIES. In: National Conference on Windtunnel Testing, July 12-14, 2007 , IIT Kanpur.

Mayuresh, - and Sudhakar, S and Ramesh, G and Sajeer, Ahmed Calibration of 0.2m low speed wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.

Mukund, R and Karthikeyan, N Experimental investigations and evaluation of MAV planforms. Project Report. National Aerospace Laboratories, Bangalore.

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Ramesh, G and Suriyanarayanan, P and Sudhakar, S Near Field Studies of an Elliptic Jet in a Co flow. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), 10-12 December 2009, Bangalore.

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Sajeer, Ahmed and Suriyanarayanan, P and Madhavan, KT and Ramesh, G Studies on Eppler 61 Airfoil with Gurney Flaps at Low Reynolds numbers. Project Report. NAL.

Sajeer, Ahmed and Swamy, MS Horizontal Tail And Flap Effectiveness Studies On Mig-21 M Aircraft Model. Technical Report. NAL, Bangalore.

Selvarajan, S Wind tunnel force measurements on 1/40 scale PSLV strap-on boosters. Project Report. National Aerospace Laboratories, Bangalore.

Sudhakar, S and Suriyanarayanan, P and Ramesh, G 2D-PIV Measurement in an elliptic Jet with Co-flow. In: 13th Asian Congress of Fluid Mechanics (ACFM), 17-21 December 2010, Dhaka, Bangladesh.

Suriyanarayanan, P and Madhavan, KT and Shailesh, Kumar and Sajeer, Ahmed Aerodynamic characteristics of Eppler 61 airfoil at Low Reynolds numbers. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, 2009,, Bangalore, India.

Suriyanarayanan, P and Venkatakrishnan, L PIV Measurements on an Air Blast Atomizer. In: 12th Asian Congress of Fluid Mechanics, 18-21 August 2008, Daejeon, Korea.

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Venkatakrishnan, L Investigation of high-lift flows using 2D PIV. Project Report. National Aerospace Laboratories, Bangalore.

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.