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AeroNDT 2017

9th International Symposium on NDT in Aerospace, 8-10 Nov, 2017, Xiamen, China

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Search Results: 49 in Date '2018-02-01'
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Exhibitors (2)
Dresden Intern.. 2
Title / Author(s) / Keywords
Identification of structural parameters for airfoil with external store based on response sensitivity analysis
G. Liu, Z. Lv, J. Liu, L. Wang
Department of Mechanics; Sun Yat-sen University, Guangzhou, China
Other Methods, Airfoil system, parameters identification, response sensitivity method

Modelling of ultrasonic beam propagation from an array through transversely isotropic fibre reinforced composites using Multi Gaussian beams
C. Anand2, S. Shroff, R. Groves7, R. Benedictus5
Faculty of Aerospace Engineering; Delft University of Technology (TU Delft)26, Delft, Netherlands
Laser ultrasound, Time of flight (TOF), Welding, Aerospace, Carbon fibre composite

Investigation of the Validity of the Elastic Kirchhoff Approximation for Rough Cracks Using a Finite Element Approach
F. Shi, W. Choi4, E. Skelton6, M. Lowe25, R. Craster6
aNDE Group bDepartment of Mathematics cMechanical Engineering; Imperial College London88, London, United Kingdom
Rough crack, Scattering, Kirchhoff approximation (KA), Finite element (FE)

Study of the loaded CFRP structure degradation utilizing combination of two acoustic methods
T. Ryzhova12, I. Gulevskii1, A. Shanygin1, Y. Petronyuk23, E. Morokov23, V. Levin23
1Central Aerohydrodinamic Institute2, Zhukovsky, Moscow , Russia
2Emanuel Institute of Biochemical Physics; Russian Academy of Sciences (RAS)30, Moscow, Russia
Impulse acoustic microscopy, Acoustic emission, Carbon fiber composite, Microstructure, acoustics

Characteristics Study of Capacitive Sensor for Oil Debris Monitoring
Z. Han2, Y. Wang7, X. Qing7
School of Aerospace Engineering; Xiamen University12, Xiamen, China
Capacitive sensor, Oil debris, Characteristics, Engine

Delamination Detection in CFRP T-joint using Laser Ultrasonic Technology
J. Mao, J. Qiu5, C. Zhang3, H. Ji4
State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)52, Nanjing, China
CFRP T-joint, Laser ultrasonic technology, Delamination

Shared Excitation Based Nonlinear Ultrasound and Vibro-Thermography Nondestructive Testing
S. Chen1, Y. He18, R. Yang22, H. Zhang32, D. Zhou4
1College of Electrical and Information Engineering; Hunan University2, Changsha, China
2College of Civil Engineering; Changsha University2, Changsha, China
3School of Electronic and Information Engineering, Fuqing Branch; Fujian Normal University2, Fujian Sheng, China
4School of Mechanical Engineering; Jiangnan University, Wuxi, China
Nonlinear ultrasound, Vibro-thermography, Impact, Aerospace, Carbon fiber composite

Pre- and post-bond inspection for assuring quality of adhesive bonds of composites after thermal treatment
P. Malinowski128, M. Sawczak12, T. Wandowski113, M. Radzienski13, W. Ostachowicz244
1Institute of Fluid-Flow Machinery; Polish Academy of Sciences (PAS)38, Gdansk, Poland
2Faculty of Automotive and Construction Machinery; Warsaw University of Technology31, Warsaw, Poland
Adhesive joints, CFRP, Composite laminates, Composite materials and repairs, Composites, electromechanical impedance, NDT

Damage assessment in composite materials using full wavefield analysis
T. Wandowski113, P. Malinowski128, W. Ostachowicz244
1Institute of Fluid-Flow Machinery; Polish Academy of Sciences (PAS)38, Gdansk, Poland
2Faculty of Automotive and Construction Machinery; Warsaw University of Technology31, Warsaw, Poland
Damage assessment, Guided wave propagation (GW), Mode conversion, Terahertz spectroscopy

Lamb wave and GMM based damage monitoring and identification for composite structure
Q. Wang6, S. Ma2
School of Automation; Nanjing University10, Nanjing, China
Lamb wave, Gaussian mixture model (GMM), Statistical characteristic parameter, Principal component analysis (PCA), Damage identification

The Porosity Test Research of Graphite Material Based on Micron Scale X-ray Tomography
S. Zhuang, Y. Song, L. Wang
Xi'an Aerospace Propulsion Institute, Xi'an, China
Liquid rocket engine, Graphite material, Micron scale X-ray tomography, Internal defect, Porosity test

Modeling of contact acoustic nonlinearity for evaluating fatigue crack in metal plate
R. Wang1, Q. Wu24, F. Yu25, Y. Okabe29, K. Xiong13
1State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)52, Nanjing, China
2Institute of Industrial Science; University of Tokyo63, Tokyo, Japan
Fatigue crack, Nonlinear ultrasonics, Nondestructive testing, Contact acoustic nonlinearity

Detection of Defects in Aircraft Multi-layered Conductive Structures by IDC-MFM Method
D. Li, X. Song, J. Gao, T. Chen, J. Tu
School of Mechanical Engineering; Hubei University of Technology, Wuhan, China
Electromagnetic Testing (ET), Non-destructive testing, Defect, magnetic field, Direct current, Conductive structure

A Damage Localization Procedure Based on Sparse Reconstruction for Lamb Waves
C. Xu, Z. Yang, S. Tian2, X. Chen, H. Zuo
aSchool of Mechanical Engineering bCollaborative Innovation Center of High-end Manufacturing Equipment; Xi'an Jiaotong University13, Xi'an, China
Lamb waves, Damage localization, Sparse representation, Carbon fiber composite

Investigation of a Strain Detection Based Load Identification Method in Spacecraft Dynamic Interface
K. Bian1, X. Song1, C. Zhou1, J. Zhang1, K. Xiong23
1College of Mechanical and Electrical Engineering; Guangzhou University4, Guangzhou, China
2State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)52, Nanjing, China
Spacecraft, Dynamic interface force, Load identification, Strain detection

Electromagnetic method for measuring the coating thickness of Fiber Carbon Composites
S. Zheng1, F. Lin16, K. Song22, S. Wu3, J. Lin119
1Eddysun Electronic Co. Ltd.22, Xiamen, China
2Key Laboratory of Nondestructive Testing, Ministry of Education; Nanchang Hang Kong University17, Nanchang, China
3Aerospace Research Institute of Material & Processing Technology, Beijing, China
Carbon fiber composite material, Coating thickness, Sweep eddy current

Study on dynamic monitoring technology of aero-engine blades
J. Lin19, H. Li7, J. Zhao.
Eddysun Electronic Co. Ltd.22, Xiamen, China
Electromagnetic induction, Eddy current testing, Online monitoring, Blade

Study on monitoring technology of aircraft engine based on vibration and oil
J. Lin119, L. Chen2
1Eddysun Electronic Co. Ltd.22, Xiamen, China
2Beijing Aeronautical Technology Research Center13, Beijing, China
Oil debris, Eddy current, Vibration, On-line monitoring

A new sensing method of big bolt loosening based on RSSI factor
J. Wu, J. Zhou
Nanjing University of Science and Technology4, Nanjing, China
Bolts loosening, RFID, RSSI Factor

Failure process analysis of T-joints under tensile load by DIC experiment and numerical simulation
Y. Wang3, H. Liu, X. Ma, K. Xiong3
State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)52, Nanjing, China
CFRP T-joint, Tensile load, The cohesive zone method(CZM), Digital image correlation(DIC)

 
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