Simulating Crack Propagation of a Selected Structural Component of the PZL-130 Orlik TC-II Aircrafts
The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test
Composite Aerospace Structure Monitoring with use of Integrated Sensors
Enhancement of Damage Detectability in Aircraft Structures Using the Fusion of NDT Results
Introduction of an Individual Aircraft Tracking Program for the Polish SU-22
Evaluation of Impact Damage in Composite Structures Using Ultrasonic Testing