Greatest drawback with tail wheel undercarriage is necessity of keeping angle of incidence of wing during landing within narrow limits; two undercarriages compared on basis of moments due to landing with cross-wind when drifting aircraft is under angle of yaw to direction of movement. English abstract from Flugwehr u Technik Mar 1944 p 80-4. (See also Engrs' Digest (Brit Edition) v 5 n 8 Aug 1944 p 225-7)


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    Titel :

    Nose wheel or tail wheel undercarriage


    Weitere Titelangaben:

    Engrs' Digest (Am Edition)


    Beteiligte:
    Jaray, P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1944


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Nose wheel or tail wheel undercarriage

    Jaray, P. | Engineering Index Backfile | 1944


    Problem of nose-wheel undercarriage reactions

    Gorloff, G. | Engineering Index Backfile | 1950


    A Problem of Nose-Wheel Undercarriage Reactions

    Orloff, G. | Emerald Group Publishing | 1950


    Tail wheel or nose wheel?

    Shanley, F.R. | Engineering Index Backfile | 1936


    Helicopter wheel undercarriage sled

    SONG XIANLONG | Europäisches Patentamt | 2015

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