A simple crack closure model for prediction of fatigue crack growth rates under variable amplitude loading / by A.U. de KoningAdvanced aluminium alloy plate materials for damage tolerant aircraft structures / by W.G.J. 't Hart ... [et al.]Damage tolerance of stiffened-skin structures: prediction and experimental verification / by H. VliegerInitial imperfection survey on a cylindrical shell (C.S.E.) at the Fokker B.V. / A.W.H. KlompéStress distribution at the tip of an interface crack between an isotropic and an anisotropic material / M.L.C.E. VerbruggenInvestigation on fracture of fibre/adhesive bondlines / M.L.C.E. VerbruggenMoisture absorption of ARALL / M.L.C.E. VerbruggenLaminate stiffnesses and classical laminate theory / J.W. GunninkInvestigation on fatigue crack growth in fibre adhesive bondlines / M.L.C.E. VerbruggenAcquisition of gust statistics from aids recorded data / by J.B. de Jonge, A.J.P. van der Wekken, R. NobackFatigue crack growth in aluminium alloys / by L.B. VogelesangA new fatigue resistant material: aramide reinforced aluminium laminate (ARALL) / by L.B. Vogelesang, R. Marissen, J. SchijveFinite element analyses of cracks in a thin walled cylinder under internal pressure / by E. Riks and P.J. den RijerLow stress intensity fatigue crack growth in 2024-T3 and T351 / by R.J.H. WanhillFatigue crack growth in ARALL : a hybrid aluminium-aramid composite material : crack growth mechanisms and quantitative predictions of the crack growth rates / Roelof MarissenCurrent status of flight simulation fatigue crack growth concepts / by R.J.H. Wanhill and J. SchijveEnvironment-assisted aerospace fatigue problems in the Netherlands / by R.J.H. WanhillQuench sensitivity of airframe aluminium alloys / by H.J. Kolkman, W.G.J. 't Hart and L. SchraBulging cracks in pressurized fuselages: a numerical study / by E. RiksFatigue damage in composites under different loading conditions / by W.G.J. 't HartWISPER: a standardized fatigue load sequence for HAWT-blades / by A.A. ten HaveStatische en damage tolerance beproeving van Fokker 100 stabilo / door H. VliegerNatuurkunde en het vliegtuig / J.L. de RoosThe blunt notch behaviour of metal laminates: ARALL and GLARE / C.A.J.R. VermeerenTime temperature relations during rubber forming continuous fiber reinforced thermoplastics / L.G. MeyersShort and long fatigue crack growth in 2024-T3 under Fokker 100 spectrum loading / by R.J.H. Wanhill and L. SchraAerodynamic measurements on a 1/5 scale model of the Fokker 50 propeller and comparison with theoretical predictions / by J.W. Kooi and W.B. de WolfThe role of experiments in improving the computational models for composite shells / J. Arbocz, J.M.A.M. HolSuperplasticity / H.E.N. BerseePreliminary results of tensile tests on single fiber bundles / L.G. MeyersCorrosion fatigue crack arrest in aluminium alloys / by R.J.H. Wanhill and L. SchraGuidelines for carbon and other advanced fibre prepreg procurement specifications / prepared by: Structures and Mechanisms Division, European Space Research and Technology CentreDamage tolerance of a postbuckling soft skin hat stiffened compression panel / by J. OlthoffIn-service detection of impact damage in composite materials / by J.H. HeidaNumerical aspects of shell stability analysis / by E. Riks, F.A. Brogan and C.C. RankinDelamination growth in improved carbon composites under constant amplitude fatigue loading / by W.G.J. 't Hart and R.H.W.M. FrijnsThermal shock and oxidation resistance of ceramic coatings / by J.A.M. Boogers, R.J.H. Wanhill and H.J.C. HersbachThe two-bay crack problem in fuselages built in GLARE and ARALL / K.J.J.M. ZaalVoorraadmodel mutatiedelen KLM/MA / P.J.L.C. Trommar JrSpacecraft sustained load fracture control / by R.J.H. Wanhill