| New approach to finite-state modeling of unsteady aerodynamics C Venkatesan, PP Friedmann AIAA journal 24 (12), 1889-1897, 1986 | 70 | 1986 |
| Fundamentals of helicopter dynamics C Venkatesan CRC Press, 2014 | 44 | 2014 |
| Electro-thermo-elastic formulation for the analysis of smart structures SN Ahmad, CS Upadhyay, C Venkatesan Smart materials and structures 15 (2), 401, 2006 | 40 | 2006 |
| Structural dynamic analysis of composite beams JK Suresh, C Venkatesan, V Ramamurti Journal of sound and vibration 143 (3), 503-519, 1990 | 35 | 1990 |
| Chaotic response of an airfoil due to aeroelastic coupling and dynamic stall V Laxman, C Venkatesan AIAA journal 45 (1), 271-280, 2007 | 32 | 2007 |
| Linear and nonlinear analysis of a smart beam using general electrothermoelastic formulation SN Ahmad, CS Upadhyay, C Venkatesan AIAA journal 42 (4), 840-849, 2004 | 30 | 2004 |
| A new aeroelastic model for composite rotor blades with straight andswept tips KA Yuan, P FRIEDMANN, C Venkatesan 33rd Structures, Structural Dynamics and Materials Conference, 2259, 1992 | 30 | 1992 |
| Free out-of-plane vibrations of a rotating beam with non-linear elastomeric constraints G Pohit, AK Mallik, C Venkatesan Journal of sound and vibration 220 (1), 1-25, 1999 | 27 | 1999 |
| Aeroelastic behavior of composite rotor blades with swept tips KA Yuan, PP Friedmann, C Venkatesan AHS, 48th Annual Forum 2, 1039-1059, 1992 | 27 | 1992 |
| Development of a structural optimization capability for the aeroelastic tailoring of composite rotor blades with straight and swept tips P Friedmann, C Venkatesan, K Yuan 4th Symposium on Multidisciplinary Analysis and Optimization, 4779, 1992 | 23 | 1992 |
| Aeroelastic effects in multi-rotor vehicles with application to a hybrid heavy lift system. Part 1: Formulation of equations of motion C Venkatesan, P Friedman NASA, 1984 | 19 | 1984 |
| Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results PP Friedmann, C Venkatesan Journal of Aircraft 22 (2), 148-155, 1985 | 18 | 1985 |
| Coupled rotor-fuselage vibration reduction using open-loop blade pitch control I Papavassiliou, PP Friedmann, C Venkatesan Mathematical and computer modelling 18 (3-4), 131-156, 1993 | 17 | 1993 |
| A new sensitivity analysis for structural optimization of composite rotor blades C Venkatesan, PP Friedmann, KA Yuan Mathematical and computer modelling 19 (3-4), 1-25, 1994 | 16 | 1994 |
| Finite state modelling of unsteady aerodynamics and its application to a rotor dynamic problem PP Friedmann, C Venkatesan | 16 | 1985 |
| Harmonic response of a shock mount employing dual-phase damping RK C Venkatesan Journal of Sound and vibration 40 (3), 409-413, 1975 | 15 | 1975 |
| Influence of unsteady aerodynamic models on aeromechanical stability in ground resonance PP Friedmann, C Venkatesan Journal of the American Helicopter Society 31 (1), 65-74, 1986 | 14 | 1986 |
| Non-linear flapping vibrations of rotating blades C Venkatesan, VT Nagaraj Journal of Sound and Vibration 84 (4), 549-556, 1982 | 14 | 1982 |
| Experimental performance evaluation of coaxial rotors for a micro aerial vehicle P Singh, C Venkatesan Journal of aircraft 50 (5), 1465-1480, 2013 | 13 | 2013 |
| Elastomeric damper model and limit cycle oscillation in bearingless helicopter rotor blade G Pohit, C Venkatesan, AK Mallik Journal of aircraft 37 (5), 923-926, 2000 | 13 | 2000 |
