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title: Fatigue of Aircraft Structures, Vol 2015, Iss 7, Pp 61-65 (2015)
Preparation of Samples used in Fatigue Testing of Aircraft Materials
Nonlinear Fatigue Damage Accumulation
The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test
The Effect of Superalloy Structure on Ultrasonic Wave Parameters
The Application of Acoustic Anisotropy to Evaluation of Material Properties
The Effect of Environmental Flight Conditions on Damage Propagation in Composite Sandwich Structure
The Impact of Damage in Inconel 718 on Hardness Measured by the Vickers Method
The Verification of the Technical Conditions of a Combat-Trainer Jet’s Airframe
Conception of New Air Target SZERSZEŃ-2
Internal Round Robin Tests for Operators of Mechanical Tests
Composite Aerospace Structure Monitoring with use of Integrated Sensors