Pages that link to "Item:Q1016267"
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The following pages link to Fatigue damage in aircraft structures, not wanted, but tolerated? (Q1016267):
Displaying 15 items.
- `WFD' - what is it and what's `LOV' got to do with it? (Q1016269) (← links)
- Eurofighter a safe life aircraft in the age of damage tolerance (Q1016273) (← links)
- Damage tolerance of bonded aircraft structures (Q1016275) (← links)
- Application of damage tolerance principles to the design of helicopters (Q1016279) (← links)
- Ensuring structural damage tolerance of russian aircraft (Q1016285) (← links)
- Fatigue crack growth history in damage tolerance design of aircraft structures (Q1016289) (← links)
- Productivity with fatigue and long memory: fractional calculus approach (Q1738682) (← links)
- Fatigue effects in elastic materials with variational damage models: a vanishing viscosity approach (Q2003402) (← links)
- A general phase-field model for fatigue failure in brittle and ductile solids (Q2039079) (← links)
- Damage identification in aluminum plates based on iterative partition algorithm using waveform centroid (Q2124100) (← links)
- Multiscale aircraft fuselage fatigue analysis by the dual boundary element method (Q2420299) (← links)
- Fatigue and damage tolerance issues of Glare in aircraft structures (Q2506556) (← links)
- Asymptotic decomposition in the problem of joined elastic plates (Q2799062) (← links)
- Mooring system design optimization using a surrogate assisted multi-objective genetic algorithm (Q5059204) (← links)
- A microelement plastic strain accumulation model for fatigue life prediction (Q6599050) (← links)