Improving the Accuracy of Fatigue Damage Calculations for Archived Data
Conception of Modular Test Stand for Fatigue Testing of Aeronautical Structures
The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test
Introduction of an Individual Aircraft Tracking Program for the Polish SU-22
Impact of Carbon Nanotubes on the Mechanical and Electrical Properties of Silicone
Composite Aerospace Structure Monitoring with use of Integrated Sensors
Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions
Model-Based Structural Integrity Assessment of Helicopter Fuselage During Harsh Landing
Model-Based Structural Integrity Assessment of Helicopter Fuselage During Harsh Landing