;Contents: Aspects of aeronautical fatigue; Methods of stress-measurement analysis for fatigue life evaluation; The use of counting accelerometer data in fatigue life predictions for aircraft flying in complex roles; The use of fracture mechanics principles in the design and analysis of damage tolerant aircraft structures; Corrosion fatigue - or - how to replace the full-scale fatigue test; On fatigue analysis and testing for the design of the airframe; A rational analytic theory of fatigue - revisited; A summary of crack growth prediction techniques; The R.Ae.S. - ESDU cumulative damage hypothesis; Fatigue life prediction - a somewhat optimistic view of the problem.
Fatigue Life Prediction for Aircraft Structures and Materials
1973
214 pages
Report
Keine Angabe
Englisch
Fatigue life prediction for aircraft structures and materials
TIBKAT | 1973
|Fatigue of aircraft materials and structures
Tema Archiv | 1994
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