Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance

Preliminary aeroelastic design of composite wings subjected to critical gust loads

Dynamic aeroelastic tailoring of a strut braced wing including fatigue loads

The influence of starter notches on flight simulation fatigue crack growth

Damage tolerance property comparisons for 2000 and 8000 series aluminium plate alloys

Re-analysis of European flight load data

WISPER and WISPERX Final definition of two standardised fatigue loading sequences for wind turbine blades

The deterministic power-spectral-density-method for linear systems

Ageing aircraft research in The Netherlands

The response of aircraft to two-dimensional vertical turbulence

Fatigue damage in composites under different loading conditions

Statistical properties of atmospheric turbulence relevant to the calculation of airplane loads

Review and comparison of discrete and continuous gust methods for the determination of airplane design loads

The tail of the test spectrum: The effect of different approximations of the lower end of a gust load spectrum on crack growth and fatigue life in 7075-T6 and 2024-T3 specimens

The effect of sheet thickness and laminating on the fatigue resistance of the aluminium alloyd AL-7010T73651

Engineering property comparisons of the aluminium plate alloys 7050-T7365I, 7010-T7365I and 7010-T765I

The influence of different types of anodic layers on the fatigue properties of 202U-T3 and 7056-T6 sheet material

Effects of variations in gust spectrum and ground-load level on fatigue life and crack propagation in 70T5-T6 and 202U-T3 specimens

NLR test results as a database to be used in a check of crack propagation prediction models: A Garteur activity

A simple analytical model for computation of specimen compliance and effective crack extension force in a centrally cracked strip, including effects of yielding