03.4 - Applied Aerodynamics
ESTIMATION OF THREE-DIMENSIONAL BOUNDARY LAYER VELOCITY PROFILES ON SWEPT WINGS AND BLENDED WING BODIES
K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom
The aim of this study is to find the most appropriate method to predict accurately the 3D boundary layer velocity profiles rn(including boundary layer skewness) on a Blended Wing Body, using boundary layer integral parameters calculated by thernrapid Viscous Full Potential method.