Improving the Accuracy of Fatigue Damage Calculations for Archived Data
Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions
The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test
Impact of Carbon Nanotubes on the Mechanical and Electrical Properties of Silicone
Introduction of an Individual Aircraft Tracking Program for the Polish SU-22
Composite Aerospace Structure Monitoring with use of Integrated Sensors
Simulating Crack Propagation of a Selected Structural Component of the PZL-130 Orlik TC-II Aircrafts