03.1 - Aerodynamics – CFD Methods and Validation
NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING
H. Mohsin¹, S.A. Prince¹, D. Di Pasquale¹; ¹Cranfield University, United Kingdom
A validation study on the RAE M2155 swept wing compares numerical results with experimental boundary layer data. Free air and wind tunnel modelling approaches are assessed, revealing better accuracy with tunnel geometry included in the simulation. Additionally, Tecplot® macro boundary layer extraction was modified to include integral calculation for supporting future flow control designs.