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83 Publications
39 Journals
C. Venkatesan
Visiting Professor
Department of Mechanical Engineering
cven@iitj.ac.in (Work)
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Publications - 83
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Publications (83)
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Publications (83)
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Conferences
Development of a structural optimization capability for the aeroelastic tailoring of composite rotor blades with straight and swept tips
P.P. Friedmann
,
C. Venkatesan
and
K. Yuan
1992 | American Institute of Aeronautics and Astronautics Inc, AIAA
Conferences
Structural dynamic model of composite rotor blades undergoing moderate deflections
K.A. Yuan
,
C. Venkatesan
and
P.P. Friedmann
1992 | Publ by ASME, New York, NY, United States
Conferences
Aeroelastic behavior of composite rotor blades with swept tips
Kuo-An Yuan
,
Peretz Friedmann P.
and
C. Venkatesan
1992 | Publ by American Helicopter Soc, Alexandria, VA, United States
Articles
Structural dynamic analysis of composite beams
J.K. Suresh
,
C. Venkatesan
and
V. Ramamurti
1990
Articles
Rotor/fuselage vibration isolation studies by a floquet-harmonic iteration technique
R. Sivaramakrishnan
,
C. Venkatesan
and
T.K. Varadan
1990
Conferences
Nonlinear coupled rotor-fuselage helicopter vibration studies with higher harmonic control
P.P. Friedmann
,
C. Venkatesan
and
I. Papavassiliou
1990 | Publ by American Helicopter Soc, Alexandria, VA, United States
Conferences
NEW APPROACH TO FINITE STATE MODELLING OF UNSTEADY AERODYNAMICS.
C. Venkatesan
and
P.P. Friedmann
1986 | AIAA (CP864), New York, NY, USA
Articles
New approach to finite-state modeling of unsteady aerodynamics
C. Venkatesan
and
P.P. Friedmann
1986
Articles
INFLUENCE OF UNSTEADY AERODYNAMIC MODELS ON AEROMECHANICAL STABILITY IN GROUND RESONANCE.
Peretz Friedmann P.
and
C. Venkatesan
1986
Articles
Aeromechanical stability analysis of a hybrid heavy lift multirotor vehicle in hover
C. Venkatesan
and
P. Friedmann
1985
Articles
Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results
P.P. Friedmann
and
C. Venkatesan
1985
Conferences
FINITE STATE MODELLING OF UNSTEADY AERODYNAMICS AND ITS APPLICATION TO A ROTOR DYNAMIC PROBLEM.
P.P. Friedmann
and
C. Venkatesan
1985 | City Univ, London, Engl
Conferences
AEROMECHANICAL STABILITY ANALYSIS OF A MULTIROTOR VEHICLE MODEL REPRESENTING A HYBRID HEAVY LIFT AIRSHIP (HHLA).
C. Venkatesan
and
P.P. Friedmann
1984 | AIAA (CP845), USA AIAA 84-0987, New York, NY, USA
Articles
AEROELASTIC EFFECTS IN MULTI-ROTOR VEHICLES WITH APPLICATION TO A HYBRID HEAVY LIFT SYSTEM. PART I: FORMULATION OF EQUATIONS OF MOTION.
C. Venkatesan
and
P. Friedmann
1984
Letters
Authors' reply
C. Venkatesan
and
V.T. Nagaraj
1983
Articles
Non-linear flapping vibrations of rotating blades
C. Venkatesan
and
V.T. Nagaraj
1982
Articles
Stochastic modeling of an aircraft traversing a runway using time series analysis
C. Venkatesan
and
V. Krishnan
1981
Letters
On the axial vibrations of rotating bars
C. Venkatesan
and
V.T. Nagaraj
1981
Conferences
OPTIMIZATION OF AIRCRAFT UNDERCARRIAGES.
C. Venkatesan
and
V.T. Nagaraj
1979
Articles
Comparison of linear and nonlinear dampers for landing gears
C. Venkatesan
1978
Showing 61-80 of 83 results
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