The calculation of undercarriage landing reactions and dynamic stresses is discussed, and the merging of the two calculations under certain circumstances is proposed. ? formulation of the combined problem is outlined, and numerical examination of a simple case shows that in some cases the reaction forces are appreciably reduced by the adoption of the combined approach. Finally, a criterion is derived which could be used in the early stages of undercarriage design to predict the elicci of aircraft flexibility.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Structural Flexibility and Undercarriage Impact Loads


    Untertitel :

    The Combination of Landing Reactions and Dynamic Stresses


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.05.1959


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Structural flexibility and undercarriage impact loads

    Alexander, H.R. | Engineering Index Backfile | 1959


    Development of Undercarriage Design Loads

    Kempf, G. / Haines, G. H. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1991


    Development of Undercarriage Design Loads

    G. Kempf / G. H. Haines | NTIS | 1990


    Landing loads on Bogie undercarriage

    Foster, S. | Engineering Index Backfile | 1952


    Landing Loads on the Bogie Undercarriage

    Foster, S. | Emerald Group Publishing | 1952