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 (Am Edition) v 1 n 10 Sept 1944 p 225-7)
Nose wheel or tail wheel undercarriage
Engrs' Digest (Brit Edition)
Engineers' Digest (British Edition) ; 5 , n 8
1944
3 pages
Article (Journal)
English
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Nose wheel or tail wheel undercarriage
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