Ranjan Ganguli
Ranjan Ganguli
Viasat Inc.
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The use of Kalman filter and neural network methodologies in gas turbine performance diagnostics: a comparative study
AJ Volponi, H DePold, R Ganguli, C Daguang
J. Eng. Gas Turbines Power 125 (4), 917-924, 2003
Strength design of composite beam using gradient and particle swarm optimization
R Kathiravan, R Ganguli
Composite structures 81 (4), 471-479, 2007
Damage assessment of structures with uncertainty by using mode-shape curvatures and fuzzy logic
M Chandrashekhar, R Ganguli
Journal of Sound and Vibration 326 (3-5), 939-957, 2009
Genetic fuzzy system for damage detection in beams and helicopter rotor blades
PM Pawar, R Ganguli
Computer methods in applied mechanics and engineering 192 (16-18), 2031-2057, 2003
Free vibration and wave propagation analysis of uniform and tapered rotating beams using spectrally formulated finite elements
KG Vinod, S Gopalakrishnan, R Ganguli
International Journal of Solids and Structures 44 (18-19), 5875-5893, 2007
Structural damage detection using fuzzy cognitive maps and Hebbian learning
P Beena, R Ganguli
Applied soft computing 11 (1), 1014-1020, 2011
A survey of recent developments in rotorcraft design optimization
R Ganguli
Journal of Aircraft 41 (3), 493-510, 2004
Design optimization of composites using genetic algorithms and failure mechanism based failure criterion
GN Naik, S Gopalakrishnan, R Ganguli
Composite Structures 83 (4), 354-367, 2008
Identification of crack location and depth in a cantilever beam using a modular neural network approach
S Suresh, SN Omkar, R Ganguli, V Mani
Smart materials and structures 13 (4), 907, 2004
Uncertainty handling in structural damage detection using fuzzy logic and probabilistic simulation
M Chandrashekhar, R Ganguli
Mechanical Systems and Signal Processing 23 (2), 384-404, 2009
New rational interpolation functions for finite element analysis of rotating beams
JB Gunda, R Ganguli
International Journal of Mechanical Sciences 50 (3), 578-588, 2008
Monitoring low cycle fatigue damage in turbine blade using vibration characteristics
S Kumar, N Roy, R Ganguli
Mechanical Systems and Signal Processing 21 (1), 480-501, 2007
Optimum design of a helicopter rotor for low vibration using aeroelastic analysis and response surface methods
R Ganguli
Journal of Sound and Vibration 258 (2), 327-344, 2002
Closed-form solutions for axially functionally graded Timoshenko beams having uniform cross-section and fixed–fixed boundary condition
K Sarkar, R Ganguli
Composites Part B: Engineering 58, 361-370, 2014
A fuzzy logic system for ground based structural health monitoring of a helicopter rotor using modal data
R Ganguli
Journal of Intelligent Material Systems and Structures 12 (6), 397-407, 2001
Structural damage detection in a helicopter rotor blade using radial basis function neural networks
RRK Reddy, R Ganguli
Smart materials and Structures 12 (2), 232, 2003
Helicopter rotor blade frequency evolution with damage growth and signal processing
N Roy, R Ganguli
Journal of Sound and vibration 283 (3-5), 821-851, 2005
University of Maryland advanced rotorcraft code (UMARC) theory manual
G Bir, I Chopra, KC Kim, J Wang, E Smith, S Vellaichamy, R Ganguli, ...
UM-Aero Report, 92-02, 1992
Application of fuzzy logic for fault isolation of jet engines
R Ganguli
J. Eng. Gas Turbines Power 125 (3), 617-623, 2003
Structural damage detection using modal curvature and fuzzy logic
M Chandrashekhar, R Ganguli
Structural Health Monitoring 8 (4), 267-282, 2009
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