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pro vyhledávání: '"Shaochang MO"'
Publikováno v:
气体物理, Vol 9, Iss 4, Pp 27-38 (2024)
Since random uncertainty may cause severe aerodynamic performance fluctuations for the wing-mounted aircraft, the Gaussian process regression (GPR) surrogate model method based on was proposed. The strategy of adding sample points by active-learning
Externí odkaz:
https://doaj.org/article/ebf9c64c656e44d9a8b9fef78ea3b1b7