Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An Evaluation of Fatigue Crack Growth Prediction Methods used in Aircraft Design



    Kongress:

    Symposium; 18th, Estimation, enhancement and control of aircraft fatigue performance ; 1995 ; Melbourne; Australia



    Erscheinungsdatum :

    1995-01-01


    Format / Umfang :

    32 pages


    Anmerkungen:

    Also known as ICAF 95



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Predicting Fatigue Crack Growth on Aircraft Structures

    Smith, Bert L. / Lee, S. Y. | SAE Technical Papers | 1981


    Fatigue crack growth history in damage tolerance design of aircraft structures

    Siegl, Jan / Nedbal, Ivan / Kunz, Jiri | Tema Archiv | 2009


    Fatigue Crack Growth Prediction for an Advanced Aircraft Structure Using a New Life Prediction Model

    Lang, M. / Delaneuville, R. / Larsen, J. et al. | British Library Conference Proceedings | 1999


    Fatigue Crack Growth Prediction and Verification of Aircraft Fuselage Panels with Multiple Site Damage

    Su, Shaopu / Liao, Jianghai / Zhang, Wendong et al. | Springer Verlag | 2019