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Aero II 39 Review of Fluid Theory

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Title: Aero II 39 Review of Fluid Theory


1
Aero II 39 Review of Fluid Theory
J. E. Brandenburg EAS 3010 Spring 2007
2
Agenda
  • Review of Incompressible Viscous Flow

3
Vortex
4
Vortex
5
Vortex
6
Circulation
7
Bernoulli Equation
8
Vortex Ring Shooter
9
Downwash
10
Review of Fluid Theory
11
Molecular Theory of Gases
Ideal Gas law P nkT n molecules per unit
volume kT ? average kinetic energy per molecule
lt1/2 mVth2 gt
12
Continuity Equation
 
l     
13
Continuity Equation Cont.
which becomes as ? x ? 0.
 
l      Similar analysis can be done for the
fluxes across the other four faces to yield the
continuity equation, which can also be written
as .
14
Continuity
Water flow speeds up in smaller pipe nozzle flow
15
Force per unit volume without viscosity
16
Momentum Equation
High pressure gas
Expanding Gas flow
17
Incompressibility Condition
18
Incompressibility Condition
19
Energy Equation without viscosity
20
Energy Equation cont.
21
Force on a fluid Element in Viscous flow
No point torques allowed
22
Turbulent Transition
23
Reynolds Number
24
Transition to turbulence
At Re gt40000 flow in water pipe becomes turbulent
25
Viscosity in a Gas
?
26
Viscosity Cont.
Downward flux of y momentum
Net flux
?
Upward flux of y momentum
27
Viscosity Cont.
28
Laminar versus Turbulent flow
29
The Boundary Layer
Re??VL/?
L
L
Near surface viscous effects create a boundary
layer that grows with distance and Reynolds
number grows also
30
Turbulent Transition on a wing
31
Turbulent Transition
32
Mars Hurricane
33
Great Red Spot- Jupiter
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