Variation in load experience: A re-analysis of Fokker F27 and Foker F28 operational acceleration data

Damage tolerance analyses of bolt/nut assemblies

Aircraft corrosion and fatigue damage assessment (USAF ASIP Publication)

A stripyield model including effects of hold periods at constant load

Spacecraft sustained load fracture control

Prediction of fatigue crack growth

European approaches in standard spectrum development

Analysis of crack opening behaviour by application of a discretised strip yield model

Fatigue Rated Fastener Systems: an AGARD coordinated testing programme

Constant-amplitude and flight-simulation fatigue tests on adhesive bonded lap joint specimens of 2024-T3 sheet material

Some tests to assess the effect of crack stoppers on the fatigue life of centre-notched sheetspecimens

A check of crack propagation prediction models against test results generated under transport aircraft flight simulation loading

The use of Arall in fuselage skins

MINITWIST: A shortened version of TWIST (Transport WIng STandard Load computer programme)

Re-assessment of service life by comparative specimen tests

Flight simulation fatigue tests on lugs with holes expanded according to the split-sleeve cold work method

Effects of flight load spectrum variations on fatigue life of riveted specimens and crack propagation in sheet made of Alclad 7075-T6

The effect of gust alleviation on fatigue in 2024-T3 Alclad

Manoeuvre spectrum fatigue crack propagation in aluminium alloy sheet materials

Heat treatment studies of aluminium alloy type 7050 forgings. Interim report no. 3: Corroded-specimen fatigue tests and SCC propagation tests