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