# hw8 - 16.100 Homework Assignment 8 Due Monday November 14...

This preview shows pages 1–2. Sign up to view the full content.

This preview has intentionally blurred sections. Sign up to view the full version.

View Full Document
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: 16.100 Homework Assignment # 8 Due: Monday, November 14, 9am Reading Assignment: No new reading. Relevant reading is same as from Homework #7. Anderson, 3 rd edition: Chapter 17, pages 787 – 801 Chapter 18, pages 803 – 810 Problem 1 In this problem, you will derive the 2-D integral momentum equation for boundary layers. The start of this derivation is the incompressible, 2-D boundary layer equations: (B) (A) = ∂ ∂ + ∂ ∂ ∂ ∂ + ∂ ∂ − = ∂ ∂ + ∂ ∂ y v x u y x p y u v x u u e τ ρ where is the pressure at the edge of the boundary layer and e p y u ∂ ∂ = µ τ . a) Assuming the flow outside of the boundary layer is inviscid, irrotational flow such that Bernoulli’s equation holds, show that Equation (A) can be manipulated to: (C) 1 y x u u y u v x u u e e ∂ ∂ + ∂ ∂ = ∂ ∂ + ∂ ∂ τ ρ b) Multiply Equation (B) by u and add to Equation (C). Then, integrate the resulting equation from to to find the boundary layer integral momentum equation:...
View Full Document

## This note was uploaded on 11/06/2011 for the course AERO 100 taught by Professor Willcox during the Fall '03 term at MIT.

### Page1 / 2

hw8 - 16.100 Homework Assignment 8 Due Monday November 14...

This preview shows document pages 1 - 2. Sign up to view the full document.

View Full Document
Ask a homework question - tutors are online