Comandur Venkatesan

发表

Effect of Pretwist on Aeroelastic Response of a Rotor System with Dynamic Stall and Dynamic Wake

Vaitla Laxman, Comandur Venkatesan, 2008 .

NEW APPROACH TO FINITE STATE MODELLING OF UNSTEADY AERODYNAMICS.

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1986 .

Aeromechanical stability analysis of a multirotor vehicle with application to hybrid heavy lift helicopter dynamics

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1984 .

Correlation studies for hingeless rotors in forward flight

Peretz P. Friedmann, Kuo-An Yuan, Comandur Venkatesan, 1994 .

Formulation of a Computational Aeroelastic Model to Predict Trim and Response of a Helicopter Rotor System

Laxman Vaitla, Comandur Venkatesan, 2009 .

Dynamic Stall Models for Aeroelastic Analysis of Helicopter Rotor Blades

Vaitla Laxman, Comandur Venkatesan, 2005 .

Harmonic response of a shock mount employing dual-phase damping

Comandur Venkatesan, R. Krishnan, 1975 .

A new aeroelastic model for composite rotor blades with straight and swept tips

Peretz P. Friedmann, Kuo-An Yuan, Comandur Venkatesan, 1992 .

Development of a Computational Aeroelastic Model for a Helicopter in Level Flight and Maneuvering Conditions

Vaitla Laxman, Comandur Venkatesan, M Rohin, 2009 .

Non-linear flapping vibrations of rotating blades

Comandur Venkatesan, V. T. Nagaraj, V. T. Nagaraj, 1982 .

Aeroelastic effects in multi-rotor vehicles with application to a hybrid heavy lift system. Part 1: Formulation of equations of motion

Comandur Venkatesan, P. Friedman, C. Venkatesan, 1984 .

Fundamentals of Helicopter Dynamics

Comandur Venkatesan, 2014 .

Computational Aeroelastic Formulation for Helicopter Rotor Loads

Vaitla Laxman, Comandur Venkatesan, 2009 .

Optimization of an oleo-pneumatic shock absorber of an aircraft during landing

Comandur Venkatesan, 1977 .

A study of the polarization–electric-field nonlinear effect on the response of smart composite plates

Comandur Venkatesan, Chandra Shekhar Upadhyay, Vl Sateesh, 2010 .

Effect of Blade Geometric Parameters on Aeroelastic Response of a Helicopter Rotor System in Hover and Forward Flight

Vaitla Laxman, Comandur Venkatesan, H ByunY., 2009 .

Vibration Control of an Idealized Helicopter Model Using Piezo Stack Sensor-Actuator

Comandur Venkatesan, Rupal Singhvi, 2005 .

Comparison of Linear and Nonlinear Dampers for Landing Gears

Comandur Venkatesan, 1978 .

Flight Dynamics of Helicopter Under Steady Maneuver: Interesting Observations

Comandur Venkatesan, T. Sakthivel, C. Venkatesan, 2017 .

Nonlinear Analysis of Smart Composite Plates Including Hysteresis Effects

Comandur Venkatesan, Chandra Shekhar Upadhyay, V. L. Sateesh, 2010 .

New approach to finite-state modeling of unsteady aerodynamics

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1986 .

Thermodynamic Modeling of Hysteresis Effects in Piezoceramics for Application to Smart Structures

Comandur Venkatesan, Chandra Shekhar Upadhyay, Vadarevu Sateesh, 2007 .

Electro-thermo-elastic formulation and analysis of a smart beam

Comandur Venkatesan, Chandra Shekhar Upadhyay, Sheikh N. Ahmad, 2003, Other Conferences.

Coupled rotor-flexible fuselage vibration reduction using open loop higher harmonic control

Peretz P. Friedmann, Comandur Venkatesan, I. Papavassiliou, 1991 .

Influence of nonlinear elastomer on isolated lag dynamics and rotor/fuselage aeromechanical stability

Comandur Venkatesan, A. K. Mallik, G. Pohit, 2000 .

Chaotic Response of an Airfoil due to Aeroelastic Coupling and Dynamic Stall

Vaitla Laxman, Comandur Venkatesan, C. Venkatesan, 2007 .

Comparison of experimental coupled helicopter rotor/body stability results with a simple analytical model

Peretz P. Friedmann, Comandur Venkatesan, 1988 .

Development of a structural optimization capability for the aeroelastic tailoring of composite rotor blades with straight and swept tips

Peretz P. Friedmann, Comandur Venkatesan, K. Yuan, 1992 .

Influence of Blade Geometric Parameters on Aeroelastic Response of a Helicopter Rotor System

Vaitla Laxman, Comandur Venkatesan, Yung Hwan Byun, 2013 .

Quasi-steady prediction of coupled bending–torsion flutter under rotating stall

Comandur Venkatesan, Abhijit Kushari, S. M. Ananth, 2013 .

Aeroelastic modeling of composite rotor blades with straight and swept tips

Peretz P. Friedmann, Kuo-An Yuan, Comandur Venkatesan, 1992 .

Nonlinear coupled rotor-fuselage helicopter vibration studies with higher harmonic control

Peretz P. Friedmann, Comandur Venkatesan, I. Papavassiliou, 1990 .

Aeromechanical stability analysis of a hybrid heavy lift multirotor vehicle in hover

Peretz P. Friedmann, Comandur Venkatesan, 1985 .

Influence of Dynamic Stall and Dynamic Wake Effects on Helicopter Trim and Rotor Loads

Vaitla Laxman, Comandur Venkatesan, C. Venkatesan, 2009 .

Influence of various unsteady aerodynamic models on the aeromechanical stability of a helicopter in ground resonance

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1984 .

Influence of Dynamic Stall on Aeroelastic Response of Airfoil Applicable for Rotary-Wing Vehicles

Vaitla Laxman, Comandur Venkatesan, 2007 .

Aeroelastic Analysis of a Helicopter Rotor Blade Including Dynamic Stall and Dynamic Wake Effects

Vaitla Laxman, Comandur Venkatesan, 2007 .

Electroelastic analysis and layer-by-layer modeling of a smart beam

Comandur Venkatesan, Chandra Shekhar Upadhyay, Sheikh N. Ahmad, 2005 .

Elastomeric Damper Model and Limit Cycle Oscillation in Bearingless Helicopter Rotor Blade

Comandur Venkatesan, A. K. Mallik, G. Pohit, 2000 .

A study of coupled rotor-fuselage vibration with higher harmonic control using a symbolic computing facility

Peretz P. Friedmann, Comandur Venkatesan, I. Papavassiliou, 1990 .

General approach to modeling and analysis of smart structures

Comandur Venkatesan, Chandra Shekhar Upadhyay, C. Upadhyay, 2003, Other Conferences.

Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1985 .

Coupled rotor-fuselage vibration reduction using open-loop blade pitch control

Peretz P. Friedmann, Comandur Venkatesan, I. Papavassiliou, 1993 .

Rotor blade dynamic stall model and its influence on airfoil response

Laxman Vaitla, Comandur Venkatesan, 2006 .

Electro-thermo-elastic formulation for the analysis of smart structures

Comandur Venkatesan, Chandra Shekhar Upadhyay, Sheikh N. Ahmad, 2006 .

Structural dynamic model of composite rotor blades undergoing moderate deflections

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1992 .

Aeroelastic stability, response and loads of swept tip composite rotor blades in forward flight

Peretz Friedman, Comandur Venkatesan, C. Venkatesan, 1994 .

Coupled rotor-fuselage vibration reduction with multiple frequency blade pitch control

Peretz P. Friedmann, Comandur Venkatesan, I. Papavassiliou, 1991 .

Structural dynamic analysis of composite beams

V. Ramamurti, Comandur Venkatesan, J. K. Suresh, 1990 .

A new sensitivity analysis for structural optimization of composite rotor blades

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1993 .

Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades

Comandur Venkatesan, Abhijit Kushari, H. Pathak, 2008 .

FREE OUT-OF-PLANE VIBRATIONS OF A ROTATING BEAM WITH NON-LINEAR ELASTOMERIC CONSTRAINTS

A. K. Mallik, G. Pohit, Comandur Venkatesan, 1999 .

INFLUENCE OF UNSTEADY AERODYNAMIC MODELS ON AEROMECHANICAL STABILITY IN GROUND RESONANCE.

Peretz P. Friedmann, Comandur Venkatesan, P. Friedmann, 1986 .