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Conference Paper

Kumar, Arun A and Viswamurthy, SR and Ganguli, R (2008) Correlation of Helicopter Rotor Aeroelastic Response with HART-II Wind Tunnel Test Data. In: 34th European Rotorcraft Forum, Liverpool, UK, Liverpool.

Viswamurthy, SR and Ganguli, R (2008) Optimal Placement of Piezoelectric Actuated Trailing-Edge Flaps for Helicopter Vibration Control. In: 16th AIAA/ASME/AHS Adaptive Structures Conference Schaumburg, IL, April 7, 2008, Schaumburg, IL.

Viswamurthy, SR and Ganguli, R (2006) Experimental and Computational Investigation of Piezoelectric Actuator Hysteresis Phenomenon in Helicopter Vibration Control using Dual Trailing Edge Flaps. In: 32nd European Rotorcraft Forum, September 12-14 2006, Maastricht, Netherlands.

Journal Article

Saijal, KK and Ganguli, Ranjan and Viswamurthy, SR (2011) Optimization of Helicopter Rotor Using Polynomial and Neural Network Metamodels. In: Journal of Aircraft, 48 (2). pp. 553-566.

Kumar, Arun A and Viswamurthy, SR and Ganguli, R (2010) Correlation of helicopter rotor aeroelastic response with HART-II wind tunnel test data. In: Aircraft Engineering and Aerospace Technology, 82 (4). pp. 237-248.

Viswamurthy, SR and Ganguli, Ranjan (2008) Performance sensitivity of helicopter global and local optimal harmonic vibration controller. In: Computers & Mathematics With Applications, 56 (10). pp. 2468-2480.

Viswamurthy, SR and Ganguli, Ranjan (2008) Using the Complete Authority of Multiple Active Trailing-edge Flaps for Helicopter Vibration Control. In: Journal of Vibration and Control, 14 (8). pp. 1175-1199.

Viswamurthy, SR and Rao, AK and Ganguli, R (2007) Dynamic hysteresis of piezoceramic stack actuators used in helicopter vibration control: experiments and simulations. In: Smart Materials and Structures, 16 (4). pp. 1109-1119.

Viswamurthy, SR and Ganguli, Ranjan (2007) Modeling and compensation of piezoceramic actuator hysteresis for helicopter vibration control. In: Sensors and Actuators A: Physical, 135 (2). pp. 801-810.

Viswamurthy, SR and Ganguli, Ranjan (2006) Effect of Piezoelectric Hysteresis on Helicopter Vibration Control Using Trailing-Edge Flaps. In: Journal of Guidance, Contro, and Dynamics, 29 (5). pp. 1201-1209.