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- since 1996 -
Search Results: 15
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Publications
EWSHM 2014 (4)
EWSHM 2018 (3)
EWSHM 2012 (2)
WCNDT 2016 (2)
ECNDT 2006 (1)
WCNDT 2008 (1)
ECNDT 2010 (1)
WCNDT 2012 (1)
EWSHM 2016 (1)
Title / Author(s) / Keywords PublicationDate
2018-11 EWSHM 2018 Aerospace
In Flight Load Determination in Critical Structure Elements Based on Operational Load Monitoring System
A. Kurnyta5, W. Zieliński, P. Reymer, M. Dziendzikowski7, K. Dragan16
Air Force Institute of Technology34, Warsaw, Poland
Detection systems, Failure diagnosis, Fatigue, Military applications, Sensors

 
EWSHM 2018
Session: Aerospace
2018-11
2018-11 EWSHM 2018 Lamb waves
An approach to damage detection based on PZT sensors and Transfer Impedance method
M. Dziendzikowski7, P. Niedbala, K. Kowalczyk, A. Kurnyta5, K. Dragan16
Air Force Institute of Technology34, Warsaw, Poland
Aerospace, Detection systems, Ultrasonics

 
EWSHM 2018
Session: Lamb waves
2018-11
2018-11 EWSHM 2018 Other
Impact induced strain wave detection using a robust feature extraction method
A. Beligni1, G. Musotto1, C. Sbarufatti17, K. Dragan216, I. Di Luch1, M. Ferrario12, M. Giglio19
1aDepartment of Mechanical Engineering bElectronics, Information and Bio-Engineering Dept; Politecnico di Milano84, Milano, Italy
2Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland
Composite materials, Data processing, Detection systems, Impact, Strain

 
EWSHM 2018
Session: Other
2018-11
2016-08 EWSHM 2016 Aerospace structures: Modeling, Verification & Validation
Lamb-wave-based monitoring of the aircraft during full-scale fatigue experiment - results and conclusions
Z. Dworakowski15, K. Dragan216, T. Stepinski127, T. Uhl128
1Department of Robotics and Mechatronics; AGH- University of Science and Technology62, Krakow, Poland
2Air Force Institute of Technology34, Warsaw, Poland
neural network, aerospace, condition monitoring, guided waves (lamb waves), Temperature compensation, ANN, Aircraft, Guided waves, ANN Ensembles

 
EWSHM 2016
Session: Aerospace structures: Modeling, Verification & Validation
2016-08
2016-07 WCNDT 2016 Image processing
Improvements to image processing algorithms used for delamination damage extraction and modeling
M. Stefaniuk2, K. Dragan16
Air Force Institute of Technology34, Warsaw, Poland
Radiographic Testing (RT), Ultrasonic Testing (UT), composite, delamination, Automated Defect Recognition ADR, C-scan, defect characterization, Ultrasonic C-scan

 
WCNDT 2016
Session: Image processing
2016-07
2016-07 WCNDT 2016 Eddy Current
Numerically Enhanced Eddy Current Inspection of Corrosion Losses of Aircraft Structures
J. Szlagowska-Spychalska12, K. Dragan216, M. Dziendzikowski27
1Warsaw University of Technology31, Warsaw, Poland
2Air Force Institute of Technology34, Warsaw, Poland
Eddy Current

 
WCNDT 2016
Session: Eddy Current
2016-07
2015-02 EWSHM 2014 Damage
Voting Neural Network Classifier for Detection of Fatigue Damage in Aircrafts
Z. Dworakowski15, L. Ambrozinski18, K. Dragan2,316, T. Stepinski127, T. Uhl128
1aFaculty of Engineering bDepartment of Robotics and Mechatronics; AGH- University of Science and Technology62, Krakow, Poland
2Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland
3Instytut Techniczny Wojsk Lotniczych (ITWL), Warsaw, Poland
Neural networks, Damage detection and localization, Aircraft SHM applications

 
EWSHM 2014
Session: Damage
2015-02
2015-02 EWSHM 2014 Guided Waves
Long Term Monitoring of an Aircraft Structure During a Full Scale Fatigue Test.
K. Dragan116, M. Dziendzikowski17, A. Kurnyta15, S. Klysz1,22
1Air Force Institute of Technology34, Warsaw, Poland
2University of Warmia and Mazury, Olsztyn, Germany
Aerospace SHM applications, Theory to practice, Damage detection and localization

 
EWSHM 2014
Session: Guided Waves
2015-02
2015-02 EWSHM 2014 SHM Applications
Approach to Health Monitoring of an Aircraft Structure with Resistive Ladder Sensors During Full Scale Fatigue Test
A. Kurnyta1,25, M. Dziendzikowski17, K. Dragan116, A. Leski1
1Air Force Institute of Technology34, Warsaw, Poland
2Military University of Technology17, Warsaw, Poland
Sensors, Damage assessment, Monitoring

 
EWSHM 2014
Session: SHM Applications
2015-02
2013-04 EWSHM 2012 PCA for Signal Processing
Damage Size Estimation with Active Piezosensor Network
M. Dziendzikowski7, K. Dragan16
Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland

 
EWSHM 2012
Session: PCA for Signal Processing
2013-04
2013-04 EWSHM 2012 SHM in Aeronautics
Damage Detection in the Aircraft Structure with the Use of Integrated Sensors – SYMOST Project
K. Dragan116, M. Dziendzikowski17, T. Uhl228, L. Ambrozinski28
1Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland
2Department of Robotics and Mechatronics; AGH- University of Science and Technology62, Krakow, Poland

 
EWSHM 2012
Session: SHM in Aeronautics
2013-04
2012-07 WCNDT 2012 Electromagnetic, Eddy Current Methods
A novel approach for the Eddy Current inspection of the aerospace structures based on the signal modeling and signal processing
J. Szlagowska Spychalska1, K. Dragan216, D. Kukla33, W. Spychalski111, K. Kurzydlowski13
1Faculty of Material Science and Engenniering; Warsaw University of Technology31, Warsaw, Poland
2Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland
3Institute of Fundamental Research; Polish Academy of Sciences (PAN)12, Warsaw, Poland
Electromagnetic Testing (ET), signal processing, Finite Element Method, Eddy current, Signal Modelling

 
WCNDT 2012
Session: Electromagnetic, Eddy Current Methods
2012-07
2010-08 ECNDT 2010 Materials Characterization
Modern Approach for Composite Inspection in the Rotorcraft Industry and Rotorcraft Maintenance
K. Dragan116, G. Gora2
1Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland
2PZL SWIDNIK S.A., Swidnik, Poland
 
ECNDT 2010
Session: Materials Characterization
2010-08
2008-11 WCNDT 2008 Ultrasonic Testing
Holistic Approach for Structural Integrity Evaluation of Composite Main Rotor Blades
K. Dragan16, S. Klimaszewski2
Safety And Reliability Division; Air Force Institute of Technology34, Warsaw, Poland
Ultrasonic Testing (UT), phased array, automated ultrasonic testing, low-frequency, Visual and Optical Testing (VT/OT), D-Sight, shearography, image processing, aerospace, adhesive joint, bonding, composite, helicopter, carbon fiber reinforced plastic (CFRP), glass, honeycomb, helicopter rotor blades, delamination, adhesives, condition monitoring, defect characterization, hidden defects, Structural integrity, Quantitative, Poland, maintenance
 
WCNDT 2008
Session: Ultrasonic Testing
2008-11
2006-11 ECNDT 2006 Aerospace
In-service Flaw Detection and Quantification on the MiG-29 Composite Vertical Tail Skin
K. Dragan16, S. Klimaszewski2
Air Force Institute of Technology34, Warsaw, Poland
Ultrasonic Testing (UT), automated ultrasonic testing, C-scan, Visual and Optical Testing (VT/OT), D-Sight, automated data collection, automated data collection, aerospace, adhesive joint, carbon fiber reinforced plastic (CFRP), composite skin, composite skin, delamination, Quantitative, Poland

 
ECNDT 2006
Session: Aerospace
2006-11
   
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