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Reliability modelling for fatigue life prediction: with application to components in dynamic systems of rotorcraft
Sam Dekker
Structural Integrity & Composites
Research output
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Thesis
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Dissertation (TU Delft)
240
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Dive into the research topics of 'Reliability modelling for fatigue life prediction: with application to components in dynamic systems of rotorcraft'. Together they form a unique fingerprint.
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INIS
prediction
100%
dynamics
100%
applications
100%
reliability
100%
fatigue
100%
modeling
100%
probability
40%
randomness
40%
service life
40%
ruptures
20%
failures
20%
regulations
20%
numerical analysis
20%
manufacturers
20%
aircraft
20%
resist
20%
cracks
20%
Engineering
Service Life
100%
Random Variable ξ
100%
Fatigue Life Prediction
100%
Aircraft Manufacturer
50%
Fatigue Failure
50%
Mechanical Component
50%
Fatigue Life
50%
Induced Fatigue
50%
Static Strength
50%
Airworthiness
50%
Material Science
Mechanical Strength
100%
Rotorcraft
100%
Fatigue of Materials
100%
Crack
50%
Aircraft
50%