9.19 Because of the velocity deficit, U-u, in t the streamlines for flow past a flat plate are not the plate. This deviation can be determine displacement thickness, 8. For air blowing shown in Fig. P9.19, plot the streamline A-BU the edge of the boundary layer (y= 8, at x = is, plot y = y(x) for streamline A-B. Assume layer flow. Streamline A-B U= 1 m/s Edge of boundary layer

5:13 4GE 40% X https://www.chegg.com/homew < C Chegg Learn on the go = Chegg Open in app EN 13.37 through 13.45 Determine the reactions and draw the shear and bending moment diagrams for the structures shown in Figs. P13.37-P13.45 using the method of consistent deformations. 40 6m kN/m FIG. P13.44 120 kN·m B C DS From 008A A .4 m 4 m El = constant m Show transcribed image text This problem has been solved! You'll get a detailed solution from a subject matter expert that helps you learn core concepts. See Answer