3241.CQ4

3241.CQ4 - accelerations, constant density. (1) u 2 (...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
3241: Aerodynamics and Flight Mechanics Name: _________________ Concept Quiz #4 The purpose of this concept quiz is to examine the application momentum equation for part of a control surface analysis. The momentum equation is: ( 29 = + F dS n U U dV U dt d S V d d d d ˆ ρ What is the y-component of momentum flux across this surface? Assume steady flow, no
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: accelerations, constant density. (1) u 2 ( A)sin( )sin( ) (2) u 2 ( A)sin( )sin( ) (3) u 2 ( A)cos( )cos( ) (4) u 2 ( A)cos( )cos( ) (5) u 2 ( A)sin( )cos( ) (6) u 2 ( A)sin( )cos( ) (7) I have no idea how to do this x U n A y...
View Full Document

This note was uploaded on 02/11/2012 for the course MAE 3241 taught by Professor Staff during the Spring '11 term at FIT.

Ask a homework question - tutors are online