Abstract:Purpose
The flow topology for multi-disciplinary configuration (MULDICON) wing is very complicated and nonlinear at low to high angle of attack (AOA). This paper aims to provide the correlation between the unsteadiness and uncertainties of the flow topology and aerodynamic forces and moments above MULDICON WING at a medium to a higher AOA.
Design/methodology/approach
The experimental and computational fluid dynamics methods were used to investigate a generic MULDICON wing. During the experiment, the AOA were… Show more
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