;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.


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    Title :

    Fatigue Life Prediction for Aircraft Structures and Materials


    Publication date :

    1973


    Size :

    214 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Fatigue life prediction for aircraft structures and materials

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1973


    Fatigue of aircraft materials and structures

    Schijve, J. | Tema Archive | 1994