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.


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    Title :

    Structural Flexibility and Undercarriage Impact Loads


    Subtitle :

    The Combination of Landing Reactions and Dynamic Stresses


    Contributors:

    Published in:

    Publication date :

    1959-05-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    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