Zobrazeno 1 - 2
of 2
pro vyhledávání: '"ZHONG XiaoKun"'
Publikováno v:
Jixie qiangdu, Vol 42, Pp 960-965 (2020)
The fatigue crack initiation of the fuselage structure skin under the uniform supercharged cyclic load of 0 ～ 7. 8 Psi was experimentally studied by the self-made aircraft fuselage skin uniform supercharged fatigue simulation device. The location o
Externí odkaz:
https://doaj.org/article/222a5e5f3e604c26b7936c8c633e0e5d
