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


AeroNDT 2017 Keywords Authors & Institutions
More Publications: •AeroNDT 2016AeroNDT 2015AeroNDT 2014AeroNDT 2013AeroNDT 2012AeroNDT 2010AeroNDT 2008
Search Results: 49 in Date '2018-02-01'
Exhibitors' Results (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. Groves5, R. Benedictus4
Faculty of Aerospace Engineering; Delft University of Technology (TU Delft)22, 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. Lowe24, R. Craster6
aNDE Group bDepartment of Mathematics cMechanical Engineering; Imperial College London81, 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)28, Moscow [Russia]
Impulse acoustic microscopy, Acoustic emission, Carbon fiber composite, Microstructure, acoustics

 
Characteristics Study of Capacitive Sensor for Oil Debris Monitoring
Z. Han2, Y. Wang6, X. Qing3
School of Aerospace Engineering; Xiamen University7, 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)45, 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. Malinowski124, M. Sawczak12, T. Wandowski113, M. Radzienski13, W. Ostachowicz240
1Institute of Fluid-Flow Machinery; polish academy of sciences (PAS)29, Gdansk [Poland]
2Faculty of Automotive and Construction Machinery; Warsaw University of Technology30, 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. Malinowski124, W. Ostachowicz240
1Institute of Fluid-Flow Machinery; polish academy of sciences (PAS)29, Gdansk [Poland]
2Faculty of Automotive and Construction Machinery; Warsaw University of Technology30, 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. Wang5, S. Ma2
School of Automation; Nanjing University9, 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)45, Nanjing [China]
2Institute of Industrial Science; University of Tokyo57, 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. Tian, X. Chen, H. Zuo
aSchool of Mechanical Engineering bCollaborative Innovation Center of High-end Manufacturing Equipment; Xi'an Jiaotong University5, 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 University2, Guangzhou [China]
2State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)45, 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 Technology3, Nanjing [China]
Bolts loosening, RFID, RSSI Factor

 
Failure process analysis of T-joints under tensile load by DIC experiment and numerical simulation
Y. Wang2, H. Liu, X. Ma, K. Xiong3
State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics (NUAA)45, Nanjing [China]
CFRP T-joint, Tensile load, The cohesive zone method(CZM), Digital image correlation(DIC)

 
 
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