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Aero II

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... because it gives local vorticity of gas flow. Curl Theorem ... At end of wings vorticity does not end but spills off end of wing. Aircraft Have Turbulent Wakes ... – PowerPoint PPT presentation

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Title: Aero II


1
Aero II Fundamental Theory of Finite Wings
Lecture 20
J. E. Brandenburg EAS 3010 Spring 2007
2
Agenda
  • Vorticity
  • Rotating Cylinder
  • Kutta Jakowski Theorem
  • Kelvins Theorem and Starting Vortex
  • Wing tip Vortices

3
Vorticity and Circulation
Vorticity is important
4
Curl
5
curl
Important because it gives local vorticity of gas
flow
6
Curl Theorem
7
Circulation
8
Incompressible Inviscid Flow
9
Force per unit volume without viscosity
10
Bernoulli Equation
11
The Pressure Coefficient
12
Rankines Ellipse
13
Doublet Flow
The limiting case as source and sink separation
goes to zero
14
Cylinder in Uniform flow
15
Cylinder in Uniform Flow
The addition of a uniform plus doublet flow
16
Real Air flow
17
Flow Around Cylinder
18
Flow Around Rotating Cylinder
Vortex term
19
Pressure Field around Non Rotating Cylinder
?
20
Pressure Field around Rotating Cylinder
?
21
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22
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23
Pressure distribution
24
Kutta-Jackowski Theorem
25
Rankines Ellipse
Cylinder shape can be modified continuously
26
Approximating Flows with Vortices
Using Vortex solutions , airflow can be modeled
continuously
27
Drag Polar
Drag is proportional to lift squared
28
Trailing 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
29
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30
Kelvins Theorem
31
Kelvins Theorem
32
Kelvins Theorem
33
Trailing Vortex
At end of wings vorticity does not end but spills
off end of wing
34
Aircraft Have Turbulent Wakes
35
Starting Vortex
36
Homework 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?

37
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