Concept of undercarriage as accessory is not valid, its form being much more that of integral part of aircraft structure; to determine undercarriage size, designer has to select suitable tires, wheels and brakes for loading and brake energy requirements of machine; method is developed by means of which project engineers can assess landing gear requirements of particular design; determination of load classification number and factors to consider; example of British Messier (Dowty Rotol) undercarriage, designed to parameters described. (41335)
Undercarriage in aeroplane project design
Aircr Eng
Aircraft Engineering ; 41 , n 2 ; p 6-11
1969
6 pages
Aufsatz (Zeitschrift)
Englisch
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The Undercarriage in Aeroplane Project Design
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