Implementation of the virtual crack closure technique in engineering FE calculations A Leski Finite Elements in Analysis and Design 43 (3), 261-268, 2007 | 144 | 2007 |
In situ Barely Visible Impact Damage detection and localization for composite structures using surface mounted and embedded PZT transducers: A comparative study M Dziendzikowski, A Kurnyta, K Dragan, S Klysz, A Leski Mechanical Systems and Signal Processing 78, 91-106, 2016 | 101 | 2016 |
Inspection methods for quality control of fibre metal laminates (FML) in the aerospace components K Dragan, J Bieniaś, A Leski, A Czulak, W Hufenbach XVI Seminarium Kompozyty Teoria i praktyka, 2012 | 16 | 2012 |
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 | 15 | 2021 |
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 | 13 | 2011 |
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 | 12 | 2015 |
Structural health monitoring of composite structures with use of embedded PZT piezoelectric sensors K Dragan, M Dziendzikowski, A Kurnyta, A Leski, J Bienias Proceedings of the ECCM-16th European Conference on Composite Materials …, 2014 | 11 | 2014 |
Good practice for fatigue crack growth curves description S Kłysz, A Leski Applied Fracture Mechanics, InTech, 197-228, 2012 | 11 | 2012 |
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 | 10 | 2011 |
Approach to health monitoring of an aircraft structure with resistive ladder sensors during full scale fatigue test K Artur, M Dziendzikowski, K Dragan, A Leski EWSHM-7th European Workshop on Structural Health Monitoring, 2014 | 9 | 2014 |
Damage size estimation of the aircraft structure with use of embedded sensor network generating elastic waves M Dziendzikowski, K Dragan, A Kurnyta, S Klysz, A Leski Key Engineering Materials 598, 57-62, 2014 | 9 | 2014 |
NDE activities connected with Service Life Extension of Main Rotor Blades of Helicopters used in Polish Armed Forces K Dragan, A Leski 7th Australian Pacific Vertiflite Conference on Helicopter Technology, 9-12, 2009 | 9 | 2009 |
The Role of AFIT in the Polish Aging Military Aircraft Programs S Klimaszewski, A Leski, J Zurek Proceedings of 7th Joint FAA/DoD/NASA Conference on Aging Aircraft, New …, 2003 | 9 | 2003 |
Technological aspects of a reparation of the leading edge of helicopter main rotor blades in field conditions M Sałaciński, K Puchała, A Leski, E Szymczyk, V Hutsaylyuk, A Bednarz, ... Applied Sciences 12 (9), 4249, 2022 | 8 | 2022 |
Least squares method modification applied to the NASGRO equation S Kłysz, J Lisiecki, A Leski, T Bąkowski Journal of Theoretical and Applied Mechanics 51 (1), 3-13, 2013 | 8 | 2013 |
Evaluation of mobile, composite airfield mat A Leski, M Wesołowski, M Stefaniuk Composites Theory and Practice 12 (4), 237-244, 2012 | 8 | 2012 |
Optimization of fatigue life of the PZL-130 Orlik’s structure A Leski, S Klimaszewski, M Kurdelski Proceedings of EngOpt 2008: International Conference on Engineering …, 2008 | 8 | 2008 |
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 | 7 | 2015 |
An Algorithm of Selecting a Representative Load Sequence for a Trainer A Leski 2nd International Conference on Engineering Optimization 400, 1-8, 2010 | 6 | 2010 |
Numerical simulation to study the influence of the thickness of canopy at a bird strike A Leski, R Baraniecki, J Malachowski DS 30: Proceedings of DESIGN 2002, the 7th International Design Conference …, 2002 | 6 | 2002 |