Wireless Energy Supply to Aircraft Structural Health Monitoring Nodes Using Ultrasonic Lamb Waves
Verification of the Computed Tomography Results of Aluminum Alloy Welded Joint
The Verification of the Technical Conditions of a Combat-Trainer Jet’s Airframe
The Impact of Damage in Inconel 718 on Hardness Measured by the Vickers Method
The Impact of Damage in Anneling Inconel 718 on Hardness Measured by the Vickers Method
The Fractographic Investigation of an Aeroengine Accessory Gearbox Quill Shaft
The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System
The Effect of Environmental Flight Conditions on Damage Propagation in Composite Sandwich Structure
The Effect of Anodizing Process Parameters on the Fatigue Life of 2024-T-351-Aluminium Alloy
The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test