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Arivoli Durai
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Cited by
Year
Self-adaptive flaps on low aspect ratio wings at low Reynolds numbers
D Arivoli, I Singh
Aerospace Science and Technology 59, 78-93, 2016
282016
Experimental studies on a propelled micro air vehicle
A Durai, R Dodamani, R Antony, S Chitlur, R Gopalan, S Ahmed
29th AIAA applied aerodynamics conference, 3656, 2011
162011
Rudimentary emulation of covert feathers on low-AR wings for poststall lift enhancement
D Arivoli, I Singh, P Suriyanarayanan
AIAA Journal 58 (2), 501-516, 2020
152020
Experimental investigation of lift and drag characteristics of a typical MAV under propeller induced flow
A Durai
International Journal of Micro Air Vehicles 6 (1), 63-72, 2014
72014
Experimental studies of propeller induced flow over a typical micro air vehicle
S Sudhakar, C Kumar, D Arivoli, R Dodamani, L Venkatakrishnan
AIAA Paper 60, 2013
42013
Experimental studies of propeller induced flow over a typical micro air vehicle
S Sudhakar, C Kumar, D Arivoli, R Dodamani, L Venkatakrishnan
AIAA Paper 60, 2013
42013
Experimental studies of propeller induced flow over a typical micro air vehicle
S Senthamarai, C Kumar, A Durai, R Dodamani, L Venkatakrishnan
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2017
12017
Effect of Gurney flap on the vortex-dominated flow over low-AR wings
D Arivoli, I Singh
Experiments in Fluids 64 (4), 68, 2023
2023
Investigation of bio-inspired passive flow control techniques for MAV application
V Harikumar, I Singh, A Durai
Bulletin of the American Physical Society 63, 2018
2018
PIV Investigation of Self-Adaptive Flap on Low Aspect Ratio Wings
A Durai, I Singh, S P
55th AIAA Aerospace Sciences Meeting, 0505, 2017
2017
Self-Activated Movable Flaps on Low Aspect Ratio Wings at Low Reynolds Numbers
D Arivoli, I Singh
International Micro Air Vehicles Conference and Flight Competition, Aachen …, 2015
2015
Preliminary wind tunnel studies on Micro-Air Vehicles
D Arivoli, R Dodamani, G Ramesh, S Ahmed
National Aerospace Laboratories, 2009
2009
Pressure measurement on NASA 0416 and NAL 7025 airfoils in the 1.5 m wind tunnel
R Mukund, D Arivoli, A Chandan Kumar
National Aerospace Laboratories, 2009
2009
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