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AeroNDT 2016

8th International Symposium on NDT in Aerospace, 3-5 Nov 2016, Bangalore, India

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Table of Contents
46 Articles in
Issue: 2017-01-01
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Exhibitors (1)
Trueflaw Ltd... 1
Title / Author(s) / Keywords Session
Modelling of Elastic Wave Scattering in Polycrystalline Materials
A. Pandala2, S. Shivaprasad2, C. Krishnamurthy29, K. Balasubramaniam114
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)135, 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. Balasubramaniam114, P. Ramakrishna
a Department of Aerospace Engineering bDepartment of Mechanical Engineering cCentre for Non Destructive Evaluation (CNDE); Indian Institute of Technology Madras (IITM)135, Chennai, India
NDT-wide, computed tomography, Composite solid propellants, random packs

On Health Monitoring of Insert Joints in Spacecraft Structures
P. Kumar4, A. Ananthan5, T. Srirangaa2, K. Dakua3, S. Narayan2
ISRO Satellite Centre7, 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. Qiu17, S. Yuan24, Y. Ren6
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)55, 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 Centre7, 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. Sriranga3, H. Kumar2, A. Ananthan5, R. Behara2, C. Varghese2
Centre for Non Destructive Evaluation (CNDE); ISRO Satellite Centre7, 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)135, 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. Virkkunen125, 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 Center16, Augsburg, Germany
Draping simulation, fibre angle measurement, robotic controlled measurement

Acoustic Emission Monitoring of the Cracking Load in Composite Materials
G. Nardoni134, N. Fallahi12, P. Nardoni121, M. Turconi24, F. Monti23
1I&T Nardoni Institute35, 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. Hillmann217, F. Macher22, M. Schulze218, H. Heuer240, C. Camerini34, G. Pereira34
1 Institute of Electronic Packaging Technology; Dresden University of Technology (TU Dresden)80, Dresden, Germany
2Fraunhofer Institute for Ceramic Technology and System (IKTS)231, Dresden, Germany
3Laboratory of Non Destructive Testing Corrosion and Welding-LNDC; Federal University of Rio de Janeiro (UFRJ)51, 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. Rajagopal33, B. Srinivasan4, K. Balasubramaniam114
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)135, Chennai, India
Ultrasonic Testing (UT), Fiber Bragg Grating, Composite laminates, Ultrasonic guided mode, Shear Horizontal mode

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