Michal Dziendzikowski

发表

An Approach to Damage Detection in the Aircraft Structure with the Use of Integrated Sensors – The Symost Project

Tadeusz Uhl, Andrzej Leski, Krzysztof Dragan, 2012 .

Structural Health Monitoring of a Composite Panel Based on PZT Sensors and a Transfer Impedance Framework

Krzysztof Dragan, Michal Dziendzikowski, Patryk Niedbala, 2018, Sensors.

Bezpośrednia diagnostyka kompozytowych elementów lotniczych z wykorzystaniem struktur inteligentnych

Andrzej Leski, Michal Dziendzikowski, Krzysztof Dragan, 2015 .

The Development of the Non-Parametric Classification Models for the Damage Monitoring on the Example of the ORLIK Aircraft Structure

Tadeusz Uhl, Krzysztof Dragan, Michal Dziendzikowski, 2012 .

Localizing impact damage of composite structures with modified RAPID algorithm and non-circular PZT arrays

Krzysztof Dragan, Michal Dziendzikowski, Andrzej Katunin, 2017 .

Use of resistive ladder sensors for crack monitoring during Full Scale Fatigue Test

Krzysztof Dragan, Michal Dziendzikowski, Artur Kurnyta, 2014, 2014 IEEE Metrology for Aerospace (MetroAeroSpace).

A method to compensate non-damage-related influences on Damage Indices used for pitch-catch scheme of piezoelectric transducer based Structural Health Monitoring

Krzysztof Dragan, Michal Dziendzikowski, K. Dragan, 2016 .

Composite Diagnostics with Use of Embedded PZT Transducers—A Smart Structure Example

Andrzej Leski, Krzysztof Dragan, Michał Sałaciński, 2015 .

Damage identification in aircraft composite structures: A case study using various non-destructive testing techniques

Krzysztof Dragan, Michal Dziendzikowski, Andrzej Katunin, 2015 .

Structural health monitoring and damage detection of the helicopter main rotor blades with the structure integrated sensors

Michal Dziendzikowski, Sławomir Klimaszewski, Krzysztof Dragan, 2011 .

Fatigue Cracks Detection and Their Growth Monitoring During Fatigue Test of a Helicopter Tail Boom

Andrzej Leski, Krzysztof Dragan, Michal Dziendzikowski, 2015 .

Damage Size Estimation of the Aircraft Structure with Use of Embedded Sensor Network Generating Elastic Waves

Andrzej Leski, Krzysztof Dragan, Sylwester Kłysz, 2014 .

3D Reconstruction of Ultrasonic B-Scans for Nondestructive Testing of Composites

Claudio Sbarufatti, Krzysztof Dragan, Angelika Wronkowicz, 2016, ICCVG.

Operational Load Monitoring System Implementation for Su-22UM3K Aging Aircraft

Wojciech Zieliński, Piotr Reymer, Michal Dziendzikowski, 2017 .

Transfer Impedance Approach to Damage Detection and Localization Based on RAPID Imaging Algorithm

Krzysztof Dragan, Michal Dziendzikowski, Artur Kurnyta, 2017 .

In situ Barely Visible Impact Damage detection and localization for composite structures using surface mounted and embedded PZT transducers: A comparative study

Andrzej Leski, Krzysztof Dragan, Sylwester Kłysz, 2016 .

Comparison of Novelty Detection Methods for Detection of Various Rotary Machinery Faults

Ziemowit Dworakowski, Mateusz Heesch, Michal Dziendzikowski, 2021, Sensors.

Recommendation System for Signal Processing in SHM

Ziemowit Dworakowski, Michal Dziendzikowski, Jakub Górski, 2021, ICAISC.

Energy Correlated Damage Indices in Fatigue Crack Extent Quantification

Krzysztof Dragan, Sylwester Kłysz, Michal Dziendzikowski, 2013 .

On the mechanical response of CFRP composite with embedded optical fibre when subjected to low velocity impact and CAI tests

Claudio Sbarufatti, Marco Giglio, Krzysztof Dragan, 2017 .

LONG TERM MONITORING OF AN AIRCRAFT STRUCTURE DURING A FULL SCALE FATIGUE TEST

Krzysztof Dragan, Michal Dziendzikowski, Artur Kurnyta, 2015 .