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Ahmed, Sajeer and Sudhakar, S (2009) Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations. Project Report. National Aerospace Laboratories, Bangalore.
Arivoli, D and Dodamani, Ravi and Ramesh, G and Ahmed, Sajeer (2009) Preliminary wind tunnel studies on Micro-Air Vehicles. Project Report. National Aerospace Laboratories, Bangalore.
Madhavan, KT and Mukund, R (2009) High-speed flow visualisation using shear-sensitive liquid crystals. In: National Conference on Wind Tunnel Testing 2009-CP12, 12-14 Mar 2009, IISc., Bangalore.
Mathur, NB and Viji, M (2009) Experimental Studies on Twin Jet Afterbody-Nozzles System of Combat Aircraft Configuration. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R (2009) Overview of the experimental facilities at the Experimental Aerodynamics Division, NAL. In: National Conference on Wind Tunnel Testing (2009-IT7), 12-14 Mar 2009, IISc., Bangalore.
Mukund, R and Arivoli, D and Chandan Kumar, A (2009) Pressure measurement on NASA 0416 and NAL 7025 airfoils in the 1.5m wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Karthikeyan, N (2009) Wind Tunnel Measurements on MAV Planforms. In: MAV Workshop Challenges and Preferred Outcomes, 13 November 2008, National Aerospace Laboratories.
Ramesh, G and Sajeer, Ahmed (2009) Development of synthetic Jet Actuator for Active Flow control. Project Report. National Aerospace Laboratories, Bangalore.
Ramesh, G and Verma, SB (2009) Investigation of near Field Flow of an Elliptic Jet in a Co-flowing Outer Stream using 2D PIV. Project Report. National Aerospace Laboratories, Bangalore.
Ramesh , G and Madhavan, KT and Sajeer, Ahmed (2009) Development of smart actuators for active flow control at low reynolds number. In: MAV Workshop Challenges and Preferred Outcomes, 13 November 2008, National Aerospace Laboratories.
Sankaranarayanan, S and Ramesh, G and Roshan, Antony and Suraj, CS (2009) Advanced Research Areas for the Development of Autonomous Micro Air vehicles : An overview. In: International Symposium on opportunities and challenges facing aviation industry in indian subcontinent, 18-20, Sreenidhi Institute of Science and Technology, Hyderabad.
Sathia Narayanan, A and Ahmed, Sajeer and Viji, M (2009) Empirical Evaluation of Wall Interference Effects on a Laminar Supercritical Airfoil at Transonic Speeds. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, Bangalore.
Venkatakrishnan, L (2009) Development of a Novel Optical Flow Diagnostic Technique for Simultaneous Measurement of Velocity and Density in Fluid Flow with Density Gradients. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2009) Recent progress in flow diagnostics techniques and aeroacoustics at NAL. In: National Conference on Wind Tunnel Testing (2009-IT10), 12-14 Mar 2009, IISc., Bangalore.
Venkatakrishnan, L and Karthikeyan, N and Verma, SB (2009) Effect of spike truncation on of the acoustics of an annular aerospike Nozzle Flow. In: 30th AIAA Aerocoustics Conference, 11-13 May 2009, Miami, Florida, USA.
Venkatakrishnan, L and Suriyanarayanan, P (2009) Density field of supersonic separated flow past an afterbody nozzle using tomographic reconstruction of BOS data. Experiments in Fluids. pp. 463-473. ISSN 0723-4864
Venkatakrishnan, L and Suriyanarayanan, P and Mathur, JS (2009) Measurement of the three- Dimensional density field around an elliptic cone at Mach 2.0 using the BOS Technique. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Manisankar, C (2009) HSTDV Nozzle Contour Optimization for Enhanced Force Characteristics – Phase I. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Sudhakar, and Venkatakrishnan, L (2009) Experimental study on a jet issuing from an elliptic nozzle with cylindrical tabs. Journal of Turbulence, 11 (20). pp. 1-24.
Verma, SB and Viji, M (2009) Experimental Evaluation of Linear Plug Nozzle Flow-field. Project Report. National Aerospace Laboratories, Bangalore.