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angle of yaw apply to turbulent Assume the virtual Booth reference Booth's results boundary layer equations boundary layer growth boundary layer returned boundary layer thickness chordwise direction chordwise flow continuity equation CORNELL UNIVERSITY dimensional displacement thickness downstream drag per unit Equations II-l erence experimental results experiments Figure 21 Finite Wings flow goes straight free stream velocity function g goes straight back growth is determined growth law Hence laminar flow leading edge lift coefficients mean velocity component momentum thickness NACA TN potential flow direction pressure distribution principle does apply Reynolds number SANDPAPER TO PRODUCE sandpaper width shape parameter shearing stress shown in Figure simple sweep theory spanwise flow stagnation point static pressure streamwise direction streamwise growth strip of sandpaper swept Traversing Mechanism turbulent boundary layer turbulent flow turbulent layers turbulent stresses unswept wing unyawed plate virtual origin yawed and unyawed yawed flat plate yawed plate YAWED WINGS yawhead Young and Booth