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Piotr Reymer
Piotr Reymer
Air Force Institute of Technology
Adresă de e-mail confirmată pe itwl.pl
Titlu
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Citat de
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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
662013
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
292014
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
112015
Operational load monitoring system implementation for Su-22UM3K aging aircraft
A Kurnyta, W Zielinski, P Reymer, M Dziendzikowski
Structural Health Monitoring 2017, 2017
102017
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
102014
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
92011
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
82011
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
62021
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
62020
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
62015
Global FEM Model of combat helicopter
G Gmurczyk, P Reymer, M Kurdelski
Journal of KONES 18, 137-144, 2011
62011
Flight Loads Acquisition for PZL-130 TC-II Full-Scale Fatigue Test
P Reymer, A Leski
Fatigue of Aircraft Structures, 2011
52011
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
42016
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
42012
Validation of the FEM model of the Mi-24 tail boom and vertical stabilizer
P Reymer
Journal of KONES 18, 369-376, 2011
42011
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
22022
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
22019
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
22018
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
22014
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
22012
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