This preview shows page 1. Sign up to view the full content.
Unformatted text preview: thickness (no velocity perpendicular to the plate) flows steadily down an infinite, inclined plane. Obtain, using the Navier-Stokes equations, an expression for the flow rate per unit width in terms of , g, h, and . Assume air resistance is negligible, so that the shear stress ( yx ) at the free surface is zero. The flow is laminar. Problem 5: The three components of velocity in a flowfield are given by: u = x 2 + y 2 + z 2 , v = xy + yz + z 2 , w = - 3xz - z 2 /2 + 4 . Determine an expression for the angular velocity (rotation) vector, and find the vorticity. Is this an irrotational flow field? Problem 6: Determine the stream function corresponding to the velocity potential: = x 3 3xy 2 . Sketch the streamline = 0, which passes through the origin. Problem 7: Solve Problem 4.83 of the textbook....
View Full Document
This note was uploaded on 04/25/2010 for the course MAE 213 taught by Professor Seshadri,k during the Spring '08 term at UCSD.
- Spring '08