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pro vyhledávání: '"Shanguang Shi"'
Publikováno v:
Applied Sciences, Vol 14, Iss 11, p 4559 (2024)
This paper presents an efficient integrated multidisciplinary design optimization method for shaping a high-pressure cooling turbine blade in aero engines. This approach utilizes a novel regression/interpolation combination surrogate model (R/ICSM),
Externí odkaz:
https://doaj.org/article/8a8aa188ae0347faaafe47a10e2e65be