Introduction to Fluid Mechanics
Download
Report
Transcript Introduction to Fluid Mechanics
Introduction to Fluid Mechanics
Bellagio Fountain
© 2006 Baylor University
Slide 1
Lecture 8
Introduction to Fluid Mechanics
Approximate Running Time - 21 minutes
Distance Learning / Online Instructional Presentation
Presented by
Department of Mechanical Engineering
Baylor University
Procedures:
1. Select “Slide Show” with the menu: Slide Show|View Show (F5 key), and hit
“Enter”
2. You will hear “CHIMES” at the completion of the audio portion of each slide; hit
the “Enter” key, or the “Page Down” key, or “Left Click”
3. You may exit the slide show at any time with the “Esc” key; and you may select
and replay any slide, by navigating with the “Page Up/Down” keys, and then
hitting “Shift+F5”.
© 2006 Baylor University
Slide 2
Lecture 8 Topics
•Outline
– Measuring Devices for
Measuring Drag
– Basics of Fluid Mechanics
– Flight Characteristics of
Baseballs & Golf Balls
Dr. Carolyn Skurla
Speaking
© 2006 Baylor University
Slide 3
Lab: Drag Force Experiment
• Performing a fluid mechanics experiment
– Collect experimental data
– Perform integration of experimental data
• Equipment:
– Wind tunnel
– Cylinder
– Pressure
transducer
– Pitot-static
tube
© 2006 Baylor University
Slide 4
So, What is Fluid Mechanics?
• The study of fluids in motion
– Solid -> Can resist a shear stress by a static deformation
– Fluid -> Cannot resist a shear stress
• Any shear stress applied to a fluid will result in motion of that fluid
• There are two classes of fluids:
– Liquids
– Gases
© 2006 Baylor University
(White, 1994)
Slide 5
Thermodynamic Properties of a
Fluid
• Pressure, p
– Compression stress at a point in a fluid
– Differences, or gradients, of pressure often drive
a fluid flow
• Temperature, T
– Measure of internal energy level of a fluid
© 2006 Baylor University
Slide 6
Thermodynamic Properties of a
Fluid
• Density,
– Mass per unit volume
• Highly variable in gases (i.e., =f(p))
• Nearly constant in liquids
– Almost incompressible
g
– Assumed to be imcompressible to make
analysis easier
• Specific Weight,
kg kg m
m s m s
2
2
3
– Weight per unit volume
© 2006 Baylor University
Slide 7
2
Pressure Transducer: Manometer
• How do we measure pressure, p ?
– Change in elevation of a liquid is equivalent to a change in
pressure
• Therefore, a static column of liquid can be used to measure pressure
difference between 2 points
p2 p1 ( z1 z2 )
(White, 1994)
© 2006 Baylor University
Slide 8
Pressure Transducer: Manometer
• Manometer units are in·H2O
– How do I convert in·H2O to more standard units for pressure?
SI Units
English
1 in H O 249.09 Pa( Pascal )
2
lb
0.036126
in
2
N ( Newton)
1 Pa 1
m
kg m
1N 1
s
2
2
© 2006 Baylor University
Slide 9
Pressure – Velocity Relationship
F pA
1
1
2 A
1
F pA
2
2
y
v = Flow velocity
x
F ma
a
ds
F F F
net
1
2
dv v
dt t
m Ads Avdt
© 2006 Baylor University
Slide 10
Pressure – Velocity Relationship
2A
1
v = Flow velocity
ds
dv
p A p A m
dt
1
( p p ) v dv
V2
1
2
V1
2
dv
( p p ) A Avdt
dt
1
2
© 2006 Baylor University
V V
( p p )
2
2
2
2
1
2
1
2
Slide 11
Pitot-Static Tube
v
Static Point
s
Static Pressure, (pS )
Static Velocity, (vS)
p
v 0
0
Stagnation Point
p
S
0
Stagnation Pressure, (p0 )
Stagnation Velocity, (v0)
Differential Pressure Transducer
(Manometer)
© 2006 Baylor University
Slide 12
Pitot-Static Tubes
• ps = Static pressure (in the moving
stream)
– Nominal air pressure in atmosphere
• p0 = Stagnation pressure
– Air pressure in the pitot tube
• vs = Static velocity
2( p0 ps )
vs
– Speed of air passing the pitot tube
• Equivalent to speed of plane through the
air
• v0 = Stagnation velocity = 0
© 2006 Baylor University
Slide 13
1
2
Pitot-Static Tube Sample
Problem
Find :
v
Solution :
249.09 Pa
p p 1.2in H O
1in H O
S
0
S
2
p p 298.9 Pa
0
Given :
air 1.2
kg
m3
2
S
kg
2(298.9 Pa) m s
v
kg Pa
1.2 2
m
2
s
R' 1.2in H O
2
3
1
2
1
2
m
m
v 498.2 22.3
s
s
2
s
© 2006 Baylor University
2
Slide 14
Velocity
• When there is friction between the
fluid and the solid surface
– No slip of the fluid at the
boundary
• Velocity = 0
– A boundary layer forms near the
solid surface
• Shear stress is greatest adjacent
to the boundary layer at the
surface
(White, 1994)
© 2006 Baylor University
Slide 15
Laminar vs. Turbulent Flow
• Laminar -> smooth and steady.
• Turbulent -> fluctuating and agitated.
© 2006 Baylor University
Slide 16
Reynolds Number
• Dimensionless parameter
VL
Re
– Correlates viscous behavior of all newtonian fluids
– = density
– = viscosity
– V = characteristic velocity of flow
– L = length scale of flow
• Most important parameter in fluid mechanics
– Governs transition from laminar to turbulent flow
© 2006 Baylor University
Slide 17
This Concludes Lecture 8
© 2006 Baylor University
Slide 18