LiftingFlows

# LiftingFlows - MEM420 Aerodynamics Dr. A. Yousuff...

This preview shows pages 1–9. Sign up to view the full content.

MEM420 Aerodynamics Dr. A. Yousuff MEM/Drexel

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

View Full Document
overview yousuff Aerodynamics 2 Non-lifting flow over a cylinder Lifting flow over a cylinder Kutta-Joukowsky Theorem (L = V ) Panel Method
Uniform flow + doublet yousuff Aerodynamics 3 22 2 1 cos , 1 sin 2 , r R wi t hR V    

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

View Full Document
Non-lifting flow over a cylinder yousuff Aerodynamics 4 The Streamline = 0 (circle) separates the flow from doublet and uniform. Uniform flow over a cylinder.
observations yousuff Aerodynamics 5 0; 2 sin r V   @ , 2 2  

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

View Full Document
Uniform flow + doublet + vortex yousuff Aerodynamics 6
Stagnation points yousuff Aerodynamics 7 2 2 1 c s 0 o r R V    2 2 2 1 sin    2 2 2 2 1 44     

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

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

## This note was uploaded on 04/26/2011 for the course MEM 420 taught by Professor Ajamal during the Spring '11 term at Drexel.

### Page1 / 13

LiftingFlows - MEM420 Aerodynamics Dr. A. Yousuff...

This preview shows document pages 1 - 9. Sign up to view the full document.

View Full Document
Ask a homework question - tutors are online