C. Venkatesan
C. Venkatesan
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Cited by
Cited by
New approach to finite-state modeling of unsteady aerodynamics
C Venkatesan, PP Friedmann
AIAA journal 24 (12), 1889-1897, 1986
Fundamentals of helicopter dynamics
C Venkatesan
CRC Press, 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
Structural dynamic analysis of composite beams
JK Suresh, C Venkatesan, V Ramamurti
Journal of sound and vibration 143 (3), 503-519, 1990
Chaotic response of an airfoil due to aeroelastic coupling and dynamic stall
V Laxman, C Venkatesan
AIAA journal 45 (1), 271-280, 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
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
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
Aeroelastic behavior of composite rotor blades with swept tips
KA Yuan, PP Friedmann, C Venkatesan
AHS, 48th Annual Forum 2, 1039-1059, 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
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
Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results
PP Friedmann, C Venkatesan
Journal of Aircraft 22 (2), 148-155, 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
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
Finite state modelling of unsteady aerodynamics and its application to a rotor dynamic problem
PP Friedmann, C Venkatesan
Harmonic response of a shock mount employing dual-phase damping
RK C Venkatesan
Journal of Sound and vibration 40 (3), 409-413, 1975
Experimental performance evaluation of coaxial rotors for a micro aerial vehicle
P Singh, C Venkatesan
Journal of aircraft 50 (5), 1465-1480, 2013
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
Non-linear flapping vibrations of rotating blades
C Venkatesan, VT Nagaraj
Journal of Sound and Vibration 84 (4), 549-556, 1982
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
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