Abstract
The Common Research Model with natural laminar flow (CRM-NLF) shows promising numerical and experimental results. This work aims at understanding the aerodynamic characteristics of the CRM-NLF wing under wind-tunnel conditions. The significant effects of turbulent wedges and static aeroelastic deformation are shown. Fluid–structure coupled simulations including laminar–turbulent transition with turbulent wedges show an improved agreement with wind-tunnel data made available by NASA when both effects are considered.
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