
12 Artículos
Predicting Fatigue Crack Growth and Fatigue Life Under Variable Amplitude Loading
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Diagnostics of Composite Aircraft Structures Using Non-Destructive Tests with Thermographic, Ultrasound and Acoustic Methods
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Calculation and Experimental Verification of Residual Stresses in Riveted Joints Used in an Airframe
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Fatigue Life Assessment of Selected Structural Elements of MI-24 Helicopter
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Fatigue Life Estimation of the Tail Boom and Vertical Stabilizer of MI-24 Helicopter
y
Investigations of Some Properties of Material Samples Taken from the Aircraft Withdrawn from Service
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