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AeroNDT 2016 Keywords Authors & Institutions

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Forthcoming Publications: - 10th International Symposium on NDT in Aerospace 2018
Search Results: 46 in Date '2017-01-01'
Title / Author(s) / Keywords Session
Modelling of Elastic Wave Scattering in Polycrystalline Materials
A. Pandala2, S. Shivaprasad2, C. Krishnamurthy25, K. Balasubramaniam110
aCentre for Non Destructive Evaluation (CNDE) bDepartment of Physics cDepartment of Mechanical Engineering cCentre for Non-Destructive Evaluation and Department of Mechanical Engineering; Indian Institute of Technology Madras (IITM)128, Chennai [India]
Polycrystalline material, Parallel processing, finite difference time domain model, Voronoi Tessellations

Main Gear Box Testing for Light Utility Helicopter
B. Muralidhar, B. Rathore
Hindustan Aeronautics Limited (HAL)11, Bangalore [India]
Main Gear Box, Closed Loop Torques, Mast loads, Test stands

Experimental Validation of Random Packs for Composite Solid Propellants Using X-Ray Computed Tomography
C. Vijay, K. Raghuvarun, K. Bhargav, K. Balasubramaniam110, P. Ramakrishna
a Department of Aerospace Engineering bDepartment of Mechanical Engineering cCentre for Non Destructive Evaluation (CNDE); Indian Institute of Technology Madras (IITM)128, Chennai [India]
NDT-wide, computed tomography, Composite solid propellants, random packs

On Health Monitoring of Insert Joints in Spacecraft Structures
P. Kumar3, A. Ananthan4, T. Srirangaa2, K. Dakua3, S. Narayan
ISRO Satellite Centre6, Bangalore [India]
Visual and Optical Testing (VT/OT), shearography, health monitoring, Diagnostic technique, Insert joint, spacecraft structure

SHM - Prognostic Analysis of Crack Growth retardation in Fastener Joints with Bush around the Pin
K. Bharath1, L. Chikmath1, B. Sravan2, B. Dattaguru1
1Department of Aerospace Engineering; Jain University, Bangalore [India]
2National Aerospace Laboratories (NAL)11, Bangalore [India]
Lug joint, metallic bush, fatigue, crack initiation and crack growth

Multiple NDE methods for crack characterization on spur gear
M. Lakshmi5, A. Mondal6, M. Subbaraju2, V. Thangavelu2, S. Sreedhar4
Gas Turbine Research Establishment (GTRE)6, Bangalore [India]
Magnetic Particle Testing, Eddy Current Testing, Spur Gear, Aero Engine

Post impact damage evaluation of high velocity impacted E-glass composites using Immersion Ultrasonic C-scan technique
M. Rao1, T. Reddy2, P. Reddy22, V. Madhu23, B. Murthy12
1Advanced Systems Laboratory; ASL Advanced Systems2, Hyderabad [India]
2Defence Metallurgical Research Laboratory (DMRL)14, Hyderabad [India]
E-glass composites, ballistic impact, energy absorption, ultrasonic C-scan analysis, damage area

A Scanning Spatial-Wavenumber Filter based On-Line Damage Imaging Method of Composite Structure
L. Qiu11, S. Yuan15, Y. Ren2
Research Center of Structural Health Monitoring and Prognosis, State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)41, Nanjing [China]
Structural health monitoring, composite structure, damage imaging, Lamb wave, scanning spatial-wavenumber filter, 2-D cruciform array

Thermo Elastic Deformation Measurements on Spacecraft Components using Non contact Target- less Image Based Technique
R. Behara2, T. Srirangaa2, C. Varghese2, C. Rao, S. Pathak, P. Mathur, K. Dakua3
Satellite center; ISRO Satellite Centre6, Bangalore [India]
Data evaluation, Image Processing, Deformation measurement, Photogrammetry, Projection dots, Thermal Cycling

Application of Image based technique in Qualification testing of Spacecraft Structures & Components.
T. Sriranga2, H. Kumar2, A. Ananthan4, R. Behara2, C. Varghese2
Centre for Non Destructive Evaluation (CNDE); ISRO Satellite Centre6, Bangalore [India]
Structural Health Monitoring, Data evaluation and Image processing

Detecting Onset of Combustion Instability in Gas Turbines Through Flame Visualisation using Fiber Optic Bundle
H. Suma, J. Vasanth, B. Srinivasan4, S. Chakravarthy
aDepartment of Electrical Engineering b Department of Aerospace Engineering; Indian Institute of Technology Madras (IITM)128, Chennai [India]
Combustion instability, Fiber optic bundle, flame visualization, precursors

Model Assisted Probability of Detection for Lognormally Distributed Defects
V. Rentala13, P. Mylavarapu24, K. Gopinath22, J. Gautam14, V. Kumar26
1School of Engineering Science and Technology; University of Hyderabad6, Hyderabad [India]
2School of Engineering Science and Technology; Defence Metallurgical Research Laboratory (DMRL)14, Hyderabad [India]
Ultrasonic testing, Probability of Detection, Flat Bottom Hole, MAPOD, bootstrap confidence intervals.

Practical experiences in POD determination for airframe ET inspection
I. Virkkunen124, M. Ylitalo2
1Trueflaw Ltd.26, Espoo [Finland]
2Patria Aviation 3, Halli [Finland]
NDT-wide, Electromagnetic Testing (ET), Probability of Detection (POD), Eddy current inspection (ET)

Advances in Phased Array Ultrasonic Testing Analysis software
B. Kodumuru1, J. Amos23
1Textron Aviation, Bangalore [India]
2Textron Aviation, Wichita, KS [USA]
composites, phased array ultrasonic testing, image analysis

A novel nonlinear acoustics technique for the detection of defects in composites
A. Singh2, V. Tan2, T. Tay2, H. Lee2
Department of Mechanical Engineering; National University of Singapore4, Singapore [Singapore]
Ultrasonic Testing (UT), Other Methods, Composites, ndt, damage detection, Delaminations, nonlinear acoustics

Comparison of fibre angles between hand draped carbon fibres and draping simulation
C. Frommel3, M. Körber
Institue for Structures and Design, Center for Lightweight-Production-Technology (ZLP); Deutsches Zentrum für Luft- und Raumfahrt (DLR), German Aerospace Center13, Augsburg [Germany]
Draping simulation, fibre angle measurement, robotic controlled measurement

Acoustic Emission Monitoring of the Cracking Load in Composite Materials
G. Nardoni133, N. Fallahi12, P. Nardoni120, M. Turconi24, F. Monti23
1I&T Nardoni Institute34, Brescia [Italy]
2Leonardo Aircraft, Vengono Superiore (VA) [Italy]
delay crack load, Acoustic emissions, Carbon-epoxy composite, fracture mechanisms

Characterization of Ceramic Composites by High Frequency Eddy Current techniques
M. Kyrychenko1, S. Hillmann216, F. Macher22, M. Schulze215, H. Heuer233, C. Camerini32, G. Pereira32
1 Institute of Electronic Packaging Technology; Dresden University of Technology (TU Dresden)66, Dresden [Germany]
2Fraunhofer Institute for Ceramic Technology and System (IKTS)204, Dresden [Germany]
3Laboratory of Non Destructive Testing Corrosion and Welding-LNDC; Federal University of Rio de Janeiro (UFRJ)43, Rio de Janeiro [Brazil]
Electromagnetic Testing (ET), ndt, carbon fiber composite, X-ray, Eddy current, C/SiC

Locating Delamination in a Composite Laminate Using Nonlinear Response of Lamb Waves
N. Yelve15, M. Mitra26, P. Mujumdar23
1Deaprtment of Mechanical Engineering; Fr. C. Rodrigues Institute of Technology (FCRIT)3, Vashi, Navi Mumbai [India]
2Department of Aerospace Engineering; Indian Institute of Technology Bombay (IITB)8, Mumbai [India]
Composite laminates, Delamination, Nonlinear response of Lamb waves, Contact nonlinearity, Higher harmonics, Locating delamination, Temporal and spectral response

Investigation of anisotropic propagation of shear horizontal modes in composite laminates using fiber Bragg grating sensors
P. Ray2, P. Rajagopal32, B. Srinivasan4, K. Balasubramaniam110
aDepartment of Electrical Engineering & Centre for Non Destructive Evaluation (CNDE) bCentre for Non-Destructive Evaluation and Department of Mechanical Engineering cDepartment of Electrical Engineering c2 Centre for Non-Destructive Evaluation, Department of Mechanical Engineering; Indian Institute of Technology Madras (IITM)128, Chennai [India]
Ultrasonic Testing (UT), Fiber Bragg Grating, Composite laminates, Ultrasonic guided mode, Shear Horizontal mode

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