The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test
Composite Aerospace Structure Monitoring with use of Integrated Sensors
The Verification of the Technical Conditions of a Combat-Trainer Jet’s Airframe
Introduction of an Individual Aircraft Tracking Program for the Polish SU-22
Improving the Accuracy of Fatigue Damage Calculations for Archived Data
Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions
Impact of Carbon Nanotubes on the Mechanical and Electrical Properties of Silicone