Zobrazeno 1 - 1
of 1
pro vyhledávání: '"I. A. Keresten"'
Publikováno v:
Russian Aeronautics. 63:586-593
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 applic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::55da5dec95d110c233df580ee2921cbc
https://doi.org/10.3103/s1068799820040042
https://doi.org/10.3103/s1068799820040042
