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Abhiram, DR and Ganguli, R and Harursampath, D and Friedmann, PP (2018) Robust design of small unmanned helicopter for hover performance using taguchi method. In: Journal of Aircraft, 55 (4). pp. 1745-1752.
Siva, C and Murugan, MS and Ganguli, Ranjan (2011) Uncertainty Quantification in Helicopter Performance Using Monte Carlo Simulations. In: Journal of Aircraft, 48 (5). pp. 1503-1511.
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, Rajan and Viswanath, PR and Ramesh, ON (2008) Nose Blowing for Side Force Control on Slender Cones at High Incidence. In: Journal of Aircraft, 45 (4). pp. 1156-1166.
Murugan, Senthil and Ganguli, Ranjan and Harursampath, Dineshkumar (2008) Aeroelastic Response of Composite Helicopter Rotor with Random Material Properties. In: Journal of Aircraft, 45 (1). pp. 306-322.
Kumar, Rajan and Ganguli, Ranjan and Omkar, SN and Kumar, Vijaya M (2008) Rotorcraft Parameter Identification from Real Time Flight Data. In: Journal of Aircraft, 45 (1). pp. 333-341.
Kumar, Brijesh and Pradeep, S (2007) Proposal to Use Reaction Jets for Variable Stability Airplanes. In: Journal of Aircraft, 44 (6). pp. 2060-2063.
Mondal, Partha and Munikrishna, N and Balakrishnan, N (2007) Cartesian-Like Grids Using a Novel Grid-Stitching Algorithm for Viscous Flow Computations. In: Journal of Aircraft, 44 (5). pp. 1598-1609.
Pawar, Prashant M and Ganguli, Ranjan (2007) Fuzzy-logic-based health monitoring and residual-life prediction for composite helicopter rotor. In: Journal of Aircraft, 44 (3). pp. 981-995.
Kumar, R and Viswanath, PR and Ramesh, ON (2005) Nose bluntness for side-force control on circular cones at high incidence. In: Journal of Aircraft, 42 (5). pp. 1133-1141.
Murugan, Senthil and Ganguli, Ranjan (2005) Aeroelastic Stability Enhancement and Vibration Suppression in a Composite Helicopter Rotor. In: Journal of Aircraft, 42 (4). pp. 1013-24.
Subaschandar, N and Prabhu, A (2002) Turbulent near-wake studies behind an infinitely swept wing. In: Journal of Aircraft, 39 (2). pp. 290-295.
Kamesh, S and Pradeep, S (1999) Phugoid approximation revisited. In: Journal of Aircraft, 36 (2). pp. 465-467.
Suresh, JK and Nagabhushanam, J (1997) Response, loads, and stability of interconnected rotor-body systems. In: Journal of Aircraft, 34 (3). pp. 416-426.
Dey, J and Narasimha, R (1990) Integral method for the calculation of incompressible two-dimensional transitional boundary layers. In: Journal of Aircraft, 27 (10). pp. 859-865.
Holla, VS and Aravamudhan, MD and Rao, P Jagadeesha (1982) Force Measurements on a Reflex Cambered Delta Wing. In: Journal of Aircraft, 19 (6). pp. 417-418.
Holla, VS and Manjunatht, AR and Nagabhushanamt, J (1982) Helicopter rotor performance evaluation using oscillatory airfoil data. In: Journal of Aircraft, 19 (12). pp. 1102-1104.
Venkatesan, C and Krishnan, V (1981) Stochastic Modeling of an Aircraft Traversing a Runway Using Time Series Analysis. In: Journal of Aircraft, 18 (2). pp. 115-120.
Gaonkar, Gopal H and Peters, David A (1980) Use of Multiblade Coordinates for Helicopter Flap-Lag Stability with Dynamic Inflow. In: Journal of Aircraft, 17 (2). pp. 112-118.
Sarma, VVS and Kunhikrishnan, KV and Ramchand, K (1979) A Decision Theory Model for Health Monitoring of Aeroengines. In: Journal of Aircraft, 16 (3). pp. 222-224.
Venkatesan , C (1978) Comparison of Linear and Nonlinear Dampers for Landing Gears. In: Journal of Aircraft, 15 (10). 696-698 .
Govindaraju, SP and Holla, VS and Nigam, A and Verghese, MP (1978) Development of a vorticity meter. In: Journal of Aircraft, 15 (11). 799-800 .