Tests of polyurethane foams with negative Poisson's ratio J Lisiecki, T Błażejewicz, S Kłysz, G Gmurczyk, P Reymer, G Mikułowski physica status solidi (b) 250 (10), 1988-1995, 2013 | 66 | 2013 |
Tomographic examination of auxetic polyurethane foam structures J Lisiecki, S Kłysz, T Błażejewicz, G Gmurczyk, P Reymer physica status solidi (b) 251 (2), 314-320, 2014 | 29 | 2014 |
Full Scale Fatigue Test concept of a Su-22 fighter bomber P Reymer, A Leski, W Zielinski, K Jankowski Fatigue of Aircraft Structures 6, 79-87, 2015 | 11 | 2015 |
Operational load monitoring system implementation for Su-22UM3K aging aircraft A Kurnyta, W Zielinski, P Reymer, M Dziendzikowski Structural Health Monitoring 2017, 2017 | 10 | 2017 |
Fatigue properties of polyurethane foams, with special emphasis on auxetic foams, used for helicopter pilot seat cushion inserts J Lisiecki, D Nowakowski, P Reymer Fatigue of Aircraft Structures 2014 (6), 72-78, 2014 | 10 | 2014 |
Development of load spectrum for full scale fatigue test of a trainer aircraft A Leski, P Reymer, M Kurdelski ICAF 2011 Structural Integrity: Influence of Efficiency and Green …, 2011 | 9 | 2011 |
Flight loads acquisition for PZL-130 Orlik TCII full scale fatigue test P Reymer, A Leski Fatigue of Aircraft Structures 2011 (3), 78-85, 2011 | 8 | 2011 |
Application of operational load monitoring system for fatigue estimation of main landing gear attachment frame of an aircraft M Dziendzikowski, A Kurnyta, P Reymer, M Kurdelski, S Klysz, A Leski, ... Materials 14 (21), 6564, 2021 | 6 | 2021 |
Numerical and experimental uav structure investigation by pre-flight load test A Kurnyta, W Zielinski, P Reymer, K Dragan, M Dziendzikowski Sensors 20 (11), 3014, 2020 | 6 | 2020 |
Fatigue life assessment of PZL-130 Orlik structure–final analysis and results A Leski, M Kurdelski, P Reymer, K Dragan, M Sałaciński Proceedings of the 34th ICAF Conference and 28th ICAF Symposium, ICAF, 2015 | 6 | 2015 |
Global FEM Model of combat helicopter G Gmurczyk, P Reymer, M Kurdelski Journal of KONES 18, 137-144, 2011 | 6 | 2011 |
Flight Loads Acquisition for PZL-130 TC-II Full-Scale Fatigue Test P Reymer, A Leski Fatigue of Aircraft Structures, 2011 | 5 | 2011 |
Full scale fatigue test of the Su-22 aircraft–Assumptions, process and preliminary conclusions A Leski, P Reymer, M Kurdelski, W Zieliński, K Jankowski AIP Conference Proceedings 1780 (1), 2016 | 4 | 2016 |
Introduction of Fatigue Markers in Full Scale Fatigue Test of an Aircraft Structure A Leski, S Kłysz, J Lisiecki, G Gmurczyk, P Reymer, D Bochenek, ... Fatigue of Aircraft Structures 2012 (4), 29-37, 2012 | 4 | 2012 |
Validation of the FEM model of the Mi-24 tail boom and vertical stabilizer P Reymer Journal of KONES 18, 369-376, 2011 | 4 | 2011 |
Fatigue crack propagation estimation based on direct strain measurement during a full-scale fatigue test P Reymer, A Leski, M Dziendzikowski Sensors 22 (5), 2019, 2022 | 2 | 2022 |
UAV pre-flight structural strength verification during on-ground static load test A Kurnyta, W Zieliński, P Reymer, M Dziendzikowski, K Dragan 2019 IEEE 5th International Workshop on Metrology for AeroSpace …, 2019 | 2 | 2019 |
In flight load determination in critical structure elements based on operational load monitoring system A Kurnyta, W Zielinski, P Reymer, M Dziendzikowski, K Dragan Proceedings of the 9th European workshop on structural health monitoring …, 2018 | 2 | 2018 |
The concept of a full scale fatigue test of a SU-22 fighter bomber P Reymer, A Leski, W Zieliński, K Jankowski Fatigue of Aircraft Structures 2014 (6), 79-87, 2014 | 2 | 2014 |
Introduction of a structure integrity program for a military trainer aircraft P Reymer, A Leski, M Kurdelski 28th International Congress of the Aeronautical Sciences, 23-28, 2012 | 2 | 2012 |