The stability analysis of an airplane while rolling is much more simplified to the extent that it can be obtained for numerical data which can be put to practical use in the design of landing gear dimensions. Every landing gear type attains to a critical ground friction coefficient that decides the beginning of instability, i.e., nosing over. This study has, in addition, a certain interest for the use of wheel brakes.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Airplane stability in taxying


    Beteiligte:
    Anderlik, E (Autor:in)

    Erscheinungsdatum :

    01.09.1932


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Airplane stability

    Richardson, L.B. | Engineering Index Backfile | 1929


    Airplane speed stability

    Prouty, R.W. | Tema Archiv | 1998


    Airplane longitudinal stability

    Metcalf, A.G.B. | Engineering Index Backfile | 1937


    Diagrams of airplane stability

    Bateman, H. | Engineering Index Backfile | 1920


    Diagrams of airplane stability

    Batemen, H | NTRS | 1921