EAS4101_S11_HW7Q - b) Dv C as a function of . c) The lift...

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

View Full Document Right Arrow Icon
EAS 4101 - Aerodynamics – Spring 2011 1/1 HW#3 2/23/11, 7 th Homework 1. Problem 1: Given: A thin, symmetric, untwisted rectangular wing of AR = 6 flying at a geometric angle of attack α possessing a chord c . Find: Evaluate the fundamental equation of Prandtl’s lifting line theory at the following 4 stations along the wing: θ = π / 8, π / 4, 3 π / 8, and π / 2. a) L C as a function of .
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: b) Dv C as a function of . c) The lift slope, a. 2. Problem 7.1 from Bertins Aerodynamics for Engineers 3. Problem 7.2 from Bertins Aerodynamics for Engineers 4. Problem 7.3 from Bertins Aerodynamics for Engineers 5. Problem 7.4 from Bertins Aerodynamics for Engineers 6. Problem 7.5 from Bertins Aerodynamics for Engineers...
View Full Document

This note was uploaded on 09/05/2011 for the course EAS 4101 taught by Professor Sheplak during the Spring '08 term at University of Florida.

Ask a homework question - tutors are online