Title: Aero II
1Aero II Fundamental Theory of Finite Wings
Lecture 20
J. E. Brandenburg EAS 3010 Spring 2007
2Agenda
- Vorticity
- Rotating Cylinder
- Kutta Jakowski Theorem
- Kelvins Theorem and Starting Vortex
- Wing tip Vortices
3Vorticity and Circulation
Vorticity is important
4Curl
5curl
Important because it gives local vorticity of gas
flow
6Curl Theorem
7Circulation
8Incompressible Inviscid Flow
9Force per unit volume without viscosity
10Bernoulli Equation
11The Pressure Coefficient
12Rankines Ellipse
13Doublet Flow
The limiting case as source and sink separation
goes to zero
14Cylinder in Uniform flow
15Cylinder in Uniform Flow
The addition of a uniform plus doublet flow
16Real Air flow
17Flow Around Cylinder
18Flow Around Rotating Cylinder
Vortex term
19Pressure Field around Non Rotating Cylinder
?
20Pressure Field around Rotating Cylinder
?
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23Pressure distribution
24Kutta-Jackowski Theorem
25Rankines Ellipse
Cylinder shape can be modified continuously
26Approximating Flows with Vortices
Using Vortex solutions , airflow can be modeled
continuously
27Drag Polar
Drag is proportional to lift squared
28Trailing Vortex Cont.
Trailing vortex creates tube of rotating air of
approximate circulation ? and approximate Kinetic
energy per unit length Drag Force ½ ?V2???R2 ?
1/8? ? (2?VR)2 1/8? ? ?2 This leads to Drag
relationship D??2?(Lift)2
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30Kelvins Theorem
31Kelvins Theorem
32Kelvins Theorem
33Trailing Vortex
At end of wings vorticity does not end but spills
off end of wing
34Aircraft Have Turbulent Wakes
35Starting Vortex
36Homework 4
- 1. (30pts) If an airplane flies at 100 meters a
second and creates two wing vortices of 10
meters diameter and 40 meters a second average
rotational velocity , what is the drag force this
creates? - 2. (30pts) Using the graphs following this slide
, estimate the drag coefficient function as a
function of lift coefficient for the case of
Re6x106 ( triangles) - 3. (30pts) a pumpkin dropped from an airplane
weighs 20kg and is approximately spherical with
radius 30cm , A. what is the average suction
caused by form drag created as it falls at
terminal velocity, B. what is its approximate
terminal velocity?
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