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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    Title :

    Nose wheel or tail wheel undercarriage


    Additional title:

    Engrs' Digest (Am Edition)


    Contributors:
    Jaray, P. (author)


    Publication date :

    1944


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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