Calculation of undercarriage landing reactions and dynamic stresses; merging of two calculations under certain circumstances proposed; examination of simple case shows that in some cases reaction forces are appreciably reduced by adoption of combined approach; criterion derived could be used in early stages of undercarriage design to predict effect of aircraft flexibility.
Structural flexibility and undercarriage impact loads
Aircraft Eng
Aircraft Engineering ; 31 , n 363 ; p 126-130
1959
5 pages
Aufsatz (Zeitschrift)
Englisch
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