Surrogate-based robust design of asymmetric splitter plates for aerodynamic performance efficiency of flatback airfoils
Year: 2026
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0325553
Author: Yunus Celik
Institution: Sivas Bilim ve Teknoloji Üniversitesi
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W7148380139