In this paper, the numerical simulation approach for designing the landing gear strut for a light aircraft is presented. The problems of extension and compression of the landing gear, as well as its strength during landing, are considered. The application of the topological optimization method for determining the optimal landing gear strut shape is shown.
About the Landing Gear Design Experience for a Light Aircraft Based on Multidisciplinary Modeling
Russ. Aeronaut.
Russian Aeronautics ; 63 , 4 ; 586-593
2020-12-01
8 pages
Article (Journal)
Electronic Resource
English
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF AIRCRAFT LANDING GEAR
TIBKAT | 2021
|MULTIDISCIPLINARY DESIGN OPTIMIZATION OF AIRCRAFT LANDING GEAR
TIBKAT | 2021
|MULTIDISCIPLINARY DESIGN OPTIMIZATION OF AIRCRAFT LANDING GEAR
TIBKAT | 2021
|