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Control Volume and Reynolds Transport Theorem 10-11-2013 Final

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57:020 Fluids Mechanics Fall2013
Control Volume and Reynolds
Transport Theorem
10. 11. 2013
Hyunse Yoon, Ph.D.
Assistant Research Scientist
IIHR-Hydroscience & Engineering
University of Iowa
1
57:020 Fluids Mechanics Fall2013
Reynolds Transport Theorem (RTT)
• An analytical tool to shift from describing the
laws governing fluid motion using the system
concept to using the control volume concept
2
57:020 Fluids Mechanics Fall2013
System vs. Control Volume
• System: A collection of matter of fixed identity
– Always the same atoms or fluid particles
– A specific, identifiable quantity of matter
• Control Volume (CV): A volume in space
through which fluid may flow
– A geometric entity
– Independent of mass
3
57:020 Fluids Mechanics Fall2013
Examples of CV
Fixed CV
CV fixed at a nozzle
Moving CV
CV moving with ship
Deforming CV
CV deforming within cylinder
4
57:020 Fluids Mechanics Fall2013
Laws of Mechanics
1. Conservation of mass:
2. Conservation of linear momentum:
3. Conservation of angular momentum:
4. Conservation of Energy:
𝑑𝑑𝑑𝑑
=0
𝑑𝑑𝑑𝑑
𝐹𝐹 = π‘šπ‘šπ‘Žπ‘Ž = π‘šπ‘š
𝑀𝑀 =
𝑑𝑑𝐻𝐻
𝑑𝑑𝑑𝑑
𝑑𝑑𝑑𝑑
= 𝑄𝑄̇ − π‘Šπ‘ŠΜ‡
𝑑𝑑𝑑𝑑
𝑑𝑑𝑉𝑉
𝑑𝑑
=
π‘šπ‘šπ‘‰π‘‰
𝑑𝑑𝑑𝑑 𝑑𝑑𝑑𝑑
• The laws apply to either solid or fluid systems
• Ideal for solid mechanics, where we follow the same system
• For fluids, the laws need to be rewritten to apply to a specific region in
the neighborhood of our product (i.e., CV)
5
57:020 Fluids Mechanics Fall2013
Extensive vs. Intensive Property
Governing Differential Equations (GDE’s):
𝑑𝑑
π‘šπ‘š, π‘šπ‘šπ‘‰π‘‰, 𝐸𝐸 = 0, 𝐹𝐹, 𝑄𝑄̇ − π‘Šπ‘ŠΜ‡
𝑑𝑑𝑑𝑑
𝐡𝐡
• 𝐡𝐡 = The amount of π‘šπ‘š, π‘šπ‘šπ‘‰π‘‰, or 𝐸𝐸 contained in the
total mass of a system or a CV; Extensive property –
Dependent on mass
• 𝛽𝛽 (or 𝑏𝑏) = The amount of 𝐡𝐡 per unit mass; Intensive
property – Independent on mass
𝑑𝑑𝑑𝑑
for nonuniform 𝐡𝐡)
𝛽𝛽 or 𝑏𝑏 = 𝐡𝐡/π‘šπ‘š (=
𝑑𝑑𝑑𝑑
𝐡𝐡 = 𝛽𝛽 ⋅ π‘šπ‘š
= οΏ½ 𝛽𝛽 𝜌𝜌𝜌𝜌𝜌𝜌
οΏ½ for nonuniform 𝛽𝛽
𝑉𝑉
=𝑑𝑑𝑑𝑑
𝐸𝐸
𝑒𝑒
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57:020 Fluids Mechanics Fall2013
Fixed CV
At time 𝑑𝑑: SYS = CV
𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 𝑑𝑑 = 𝐡𝐡𝐢𝐢𝐢𝐢 (𝑑𝑑)
At time 𝑑𝑑 + 𝛿𝛿𝛿𝛿: SYS = (CV – I) + II
𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 𝑑𝑑 + 𝛿𝛿𝛿𝛿
= 𝐡𝐡𝐢𝐢𝐢𝐢 𝑑𝑑 + 𝛿𝛿𝛿𝛿 − 𝐡𝐡𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿
+ 𝐡𝐡𝐼𝐼𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿
7
57:020 Fluids Mechanics Fall2013
Time Rate of Change of 𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝛿𝛿𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 𝑑𝑑 + 𝛿𝛿𝛿𝛿 − 𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 (𝑑𝑑)
=
𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿
𝐡𝐡𝐢𝐢𝐢𝐢 𝑑𝑑 + 𝛿𝛿𝛿𝛿 − 𝐡𝐡𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿 + 𝐡𝐡𝐼𝐼𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿
=
𝛿𝛿𝛿𝛿
∴
− 𝐡𝐡𝐢𝐢𝐢𝐢 𝑑𝑑
𝛿𝛿𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 𝐡𝐡𝐢𝐢𝐢𝐢 𝑑𝑑 + 𝛿𝛿𝛿𝛿 − 𝐡𝐡𝐢𝐢𝐢𝐢 𝑑𝑑
𝐡𝐡𝐼𝐼𝐼𝐼 (𝑑𝑑 + 𝛿𝛿𝛿𝛿)
𝐡𝐡𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿
=
+
−
𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿
1) Change of 𝐡𝐡
within CV over 𝛿𝛿𝛿𝛿
2) Amount of 𝐡𝐡
flowing out
through CS
over 𝛿𝛿𝛿𝛿
Now, take limit of 𝛿𝛿𝛿𝛿 → 0 to Eq. (1) term by term
3) Amountt of 𝐡𝐡
flowing in
through CS
over 𝛿𝛿𝛿𝛿
Eq. (1)
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57:020 Fluids Mechanics Fall2013
LHS of Eq. (1)
𝛿𝛿𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 𝑑𝑑 + 𝛿𝛿𝛿𝛿 − 𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 (𝑑𝑑)
lim
= lim
=
𝛿𝛿𝛿𝛿→0 𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿→0
𝛿𝛿𝛿𝛿
𝑑𝑑𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑𝑑𝑑
Time rate of
change of 𝐡𝐡
within the
system
𝐷𝐷𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
or, =
; material derivative
𝐷𝐷𝐷𝐷
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57:020 Fluids Mechanics Fall2013
First term of RHS of Eq.(1)
𝑑𝑑
𝐡𝐡𝐢𝐢𝐢𝐢 𝑑𝑑 + 𝛿𝛿𝛿𝛿 − 𝐡𝐡𝐢𝐢𝐢𝐢 (𝑑𝑑) 𝑑𝑑𝐡𝐡𝐢𝐢𝐢𝐢
=
= οΏ½ 𝛽𝛽𝛽𝛽𝛽𝛽𝛽𝛽
𝛿𝛿𝛿𝛿→0
𝑑𝑑𝑑𝑑
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
𝛿𝛿𝛿𝛿
lim
Time rate of change of
𝐡𝐡 withich CV
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57:020 Fluids Mechanics Fall2013
2nd term of RHS of Eq.(1)
and
π›Ώπ›Ώπ‘šπ‘šπ‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = πœŒπœŒπœŒπœŒπ‘‰π‘‰
𝛿𝛿𝑉𝑉 = 𝛿𝛿𝛿𝛿 ⋅ 𝛿𝛿ℓ𝑛𝑛 = 𝛿𝛿𝛿𝛿 ⋅
𝛿𝛿𝛿
οΏ½ cos πœƒπœƒ = 𝛿𝛿𝛿𝛿 ⋅ (𝑉𝑉𝑉𝑉𝑉𝑉 cos πœƒπœƒ)
=𝑉𝑉𝑉𝑉𝑉𝑉
Thus, the amount of 𝐡𝐡 flowing out of CV through 𝛿𝛿𝛿𝛿 over a short time 𝛿𝛿𝛿𝛿:
∴ π›Ώπ›Ώπ΅π΅π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = π›½π›½π›½π›½π‘šπ‘šπ‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = 𝛽𝛽𝛽𝛽𝛽𝛽 cos πœƒπœƒ 𝛿𝛿𝛿𝛿𝛿𝛿𝛿𝛿
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57:020 Fluids Mechanics Fall2013
12
2nd term of RHS of Eq.(1) – Contd.
By integrating π›Ώπ›Ώπ΅π΅π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ over the entire outflow portion of CS,
Thus,
𝐡𝐡𝐼𝐼𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿 = οΏ½
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
π‘‘π‘‘π΅π΅π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = οΏ½
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
𝛽𝛽𝛽𝛽𝛽𝛽 cos πœƒπœƒ 𝛿𝛿𝛿𝛿𝛿𝛿𝛿𝛿
𝐡𝐡𝐼𝐼𝐼𝐼 (𝑑𝑑 + 𝛿𝛿𝛿𝛿)
1
= lim
𝛿𝛿𝛿𝛿 οΏ½
𝛽𝛽𝛽𝛽𝛽𝛽 cos πœƒπœƒ 𝑑𝑑𝑑𝑑
𝛿𝛿𝛿𝛿→0
𝛿𝛿𝛿𝛿→0 𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
lim
=οΏ½
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
οΏ½,
Note that 𝑉𝑉 cos πœƒπœƒ = 𝑉𝑉 ⋅ 𝒏𝒏
∴ 𝐡𝐡̇out = οΏ½
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
𝛽𝛽𝛽𝛽 𝑉𝑉 cos πœƒπœƒ 𝑑𝑑𝑑𝑑
=𝑉𝑉𝑛𝑛
≡ π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
i.e., Out flux of 𝐡𝐡 through CS
�𝑑𝑑𝑑𝑑
𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
π‘Žπ‘Ž ⋅ 𝑏𝑏 = π‘Žπ‘Ž 𝑏𝑏 cos πœƒπœƒ
57:020 Fluids Mechanics Fall2013
3rd term of RHS of Eq.(1)
and
𝛿𝛿𝑉𝑉 = 𝛿𝛿𝛿𝛿 ⋅ 𝛿𝛿ℓ𝑛𝑛 = 𝛿𝛿𝛿𝛿 ⋅
π›Ώπ›Ώπ‘šπ‘šπ‘–π‘–π‘–π‘– = πœŒπœŒπœŒπœŒπ‘‰π‘‰
𝛿𝛿𝛿
οΏ½
=𝑉𝑉𝑉𝑉𝑉𝑉
− cos πœƒπœƒ
<0
= 𝛿𝛿𝛿𝛿 ⋅ (−𝑉𝑉𝑉𝑉𝑉𝑉 cos πœƒπœƒ)
Thus, the amount of 𝐡𝐡 flowing out of CV through 𝛿𝛿𝛿𝛿 over a short time 𝛿𝛿𝛿𝛿:
∴ 𝛿𝛿𝐡𝐡𝑖𝑖𝑖𝑖 = π›½π›½π›½π›½π‘šπ‘šπ‘–π‘–π‘–π‘– = −𝛽𝛽𝛽𝛽𝛽𝛽 cos πœƒπœƒ 𝛿𝛿𝛿𝛿𝛿𝛿𝛿𝛿
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57:020 Fluids Mechanics Fall2013
3rd term of RHS of Eq.(1) – Contd.
By integrating π›Ώπ›Ώπ΅π΅π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ over the entire outflow portion of CS,
Thus,
𝐡𝐡𝐼𝐼 𝑑𝑑 + 𝛿𝛿𝛿𝛿 = οΏ½
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
𝑑𝑑𝐡𝐡𝑖𝑖𝑖𝑖 = οΏ½
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
−𝛽𝛽𝛽𝛽𝛽𝛽 cos πœƒπœƒ 𝛿𝛿𝛿𝛿𝛿𝛿𝛿𝛿
𝐡𝐡𝐼𝐼 (𝑑𝑑 + 𝛿𝛿𝛿𝛿)
1
= lim
𝛿𝛿𝛿𝛿 οΏ½
−𝛽𝛽𝛽𝛽𝛽𝛽 cos πœƒπœƒ 𝑑𝑑𝑑𝑑
𝛿𝛿𝛿𝛿→0
𝛿𝛿𝛿𝛿→0 𝛿𝛿𝛿𝛿
𝛿𝛿𝛿𝛿
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
lim
= −οΏ½
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
οΏ½,
Note that 𝑉𝑉 cos πœƒπœƒ = 𝑉𝑉 ⋅ 𝒏𝒏
∴ 𝐡𝐡̇in = − οΏ½
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
𝛽𝛽𝛽𝛽 𝑉𝑉 cos πœƒπœƒ 𝑑𝑑𝑑𝑑
=−𝑉𝑉𝑛𝑛
�𝑑𝑑𝑑𝑑
𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
≡ 𝐡𝐡̇𝑖𝑖𝑖𝑖
i.e., influx of 𝐡𝐡 through CS
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57:020 Fluids Mechanics Fall2013
RTT for Fixed CV
Now the relationship between the time rate of change of 𝐡𝐡 for the system
and that for the CV is given by,
𝐷𝐷𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑
�𝑑𝑑𝑑𝑑 − − οΏ½ 𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
�𝑑𝑑𝑑𝑑
= οΏ½ 𝛽𝛽𝛽𝛽𝛽𝛽𝛽𝛽 + οΏ½
𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
𝐷𝐷𝐷𝐷
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
𝐡𝐡̇𝑖𝑖𝑖𝑖
With the fact that 𝐢𝐢𝐢𝐢 = πΆπΆπ‘†π‘†π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ + 𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖 ,
𝐷𝐷𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑
�𝑑𝑑𝑑𝑑
= οΏ½ 𝛽𝛽𝛽𝛽𝛽𝛽𝛽𝛽 + οΏ½ 𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
𝐷𝐷𝐷𝐷
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
𝐢𝐢𝑆𝑆
Time rate of
change of 𝐡𝐡
within a system
=
Time rate of
change of 𝐡𝐡
within CV
+
Net flux of 𝐡𝐡
through CS
= π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ − 𝐡𝐡̇𝑖𝑖𝑖𝑖
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57:020 Fluids Mechanics Fall2013
Example 1
16
57:020 Fluids Mechanics Fall2013
Example 1 - Contd.
π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = οΏ½
πΆπΆπ‘†π‘†π‘œπ‘œπ‘’π‘’π‘’π‘’
�𝑑𝑑𝑑𝑑
πœŒπœŒπœŒπœŒπ‘½π‘½ ⋅ 𝒏𝒏
(4.16)
οΏ½ = 𝑉𝑉 cos πœƒπœƒ ,
With 𝛽𝛽= 1 and 𝑽𝑽 ⋅ 𝒏𝒏
π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = οΏ½ 𝜌𝜌𝜌𝜌 cos πœƒπœƒ 𝑑𝑑𝑑𝑑 = 𝜌𝜌𝜌𝜌 cos πœƒπœƒ οΏ½ 𝑑𝑑𝑑𝑑
𝐢𝐢𝐷𝐷
where
= 𝜌𝜌𝜌𝜌 cos πœƒπœƒ 𝐴𝐴𝐢𝐢𝐢𝐢
𝐴𝐴𝐢𝐢𝐢𝐢 = β„“ × (2 π‘šπ‘š)
=
0.5 π‘šπ‘š
cos πœƒπœƒ
2 π‘šπ‘š =
𝐢𝐢𝐷𝐷
=𝐴𝐴𝐢𝐢𝐢𝐢
1
π‘šπ‘š2
cos πœƒπœƒ
17
57:020 Fluids Mechanics Fall2013
Example 1 - Contd.
Thus, with 𝜌𝜌 = 1,000 kg/m3 for water and 𝑉𝑉 = 3 m/s,
π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = 1,000
kg
m3
m
1
3
cos πœƒπœƒ
m2 = 3,000 kg/s
s
cos πœƒπœƒ
With 𝛽𝛽 = 1/𝜌𝜌,
π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = οΏ½ 𝑉𝑉 cos πœƒπœƒ 𝑑𝑑𝑑𝑑 = 𝑉𝑉 cos πœƒπœƒ οΏ½ 𝑑𝑑𝑑𝑑 = 𝑉𝑉 cos πœƒπœƒ 𝐴𝐴𝐢𝐢𝐢𝐢
𝐢𝐢𝐷𝐷
𝐢𝐢𝐷𝐷
=𝐴𝐴𝐢𝐢𝐢𝐢
=1/ cos πœƒπœƒ
m
1
= 3
cos πœƒπœƒ
m2 = 3 m3 ⁄s (𝑖𝑖. 𝑒𝑒. , volume flow rate)
cos πœƒπœƒ
s
Note: These results are the same for all πœƒπœƒ values
18
57:020 Fluids Mechanics Fall2013
19
Special Case:
𝑉𝑉= constant over discrete CS’s
𝐡𝐡̇𝑖𝑖𝑖𝑖 = οΏ½
𝐢𝐢𝑆𝑆𝑖𝑖𝑖𝑖
π΅π΅Μ‡π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ = οΏ½
οΏ½ 𝑑𝑑𝑑𝑑 = οΏ½ 𝛽𝛽𝑖𝑖 πœŒπœŒπ‘–π‘– 𝑉𝑉𝑖𝑖 𝐴𝐴𝑖𝑖
𝛽𝛽𝛽𝛽 𝑉𝑉�
⋅ 𝒏𝒏
πΆπΆπ‘†π‘†π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
οΏ½ 𝑑𝑑𝑑𝑑 = οΏ½ 𝛽𝛽𝑗𝑗 πœŒπœŒπ‘—π‘— 𝑉𝑉𝑗𝑗 𝐴𝐴𝑗𝑗
𝛽𝛽𝛽𝛽 𝑉𝑉�
⋅ 𝒏𝒏
𝐷𝐷𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑
∴
= οΏ½ 𝛽𝛽𝛽𝛽𝛽𝛽𝛽𝛽 + οΏ½ 𝛽𝛽𝑗𝑗 πœŒπœŒπ‘—π‘— 𝑉𝑉𝑗𝑗 𝐴𝐴𝑗𝑗
𝐷𝐷𝐷𝐷
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
𝑗𝑗
𝑖𝑖
constant
𝑖𝑖𝑖𝑖
π‘šπ‘šΜ‡π‘—π‘—
𝑗𝑗
constant
π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
− οΏ½ 𝛽𝛽𝑖𝑖 πœŒπœŒπ‘–π‘– 𝑉𝑉𝑖𝑖 𝐴𝐴𝑖𝑖
𝑖𝑖
π‘šπ‘šΜ‡π‘–π‘–
𝑖𝑖𝑖𝑖
π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
57:020 Fluids Mechanics Fall2013
Example 2
Given:
• Water flow (𝜌𝜌 = constant)
• 𝐷𝐷1 = 10 cm; 𝐷𝐷2 = 15 cm
• 𝑉𝑉1 = 10 cm/s
• Steady flow
Find: 𝑉𝑉2 = ?
Mass conservation:
• 𝐷𝐷𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠 /𝐷𝐷𝐷𝐷 = 0
• 𝛽𝛽 = 1
• 𝜌𝜌1 = 𝜌𝜌2 = 𝜌𝜌
𝜌𝜌1 𝐴𝐴1
𝜌𝜌
∴ 𝑉𝑉2 =
𝑉𝑉1 =
𝜌𝜌2 𝐴𝐴2
𝜌𝜌
Steady flow
0=
𝑑𝑑
οΏ½ 𝜌𝜌𝜌𝜌𝜌𝜌 + 𝜌𝜌2 𝑉𝑉2 𝐴𝐴2 − 𝜌𝜌1 𝑉𝑉1 𝐴𝐴1
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
or, 𝜌𝜌1 𝑉𝑉1 𝐴𝐴1 = 𝜌𝜌2 𝑉𝑉2 𝐴𝐴2
𝐷𝐷1
𝐷𝐷2
2
𝑉𝑉1 = 1
10 cm
15 cm
2
10
cm
= 4.4 cm/s
s
20
57:020 Fluids Mechanics Fall2013
Example 3
Given:
• 𝐷𝐷1 = 5 cm; 𝐷𝐷2 = 7 cm
• 𝑉𝑉1 = 3 m/s
• 𝑄𝑄3 = 𝑉𝑉3 𝐴𝐴3 = 0.01 m3/s
• β„Ž = constant (i.e., steady flow)
• 𝜌𝜌1 = 𝜌𝜌2 = 𝜌𝜌3 = 𝜌𝜌water
Find: 𝑉𝑉2 = ?
= 0; steady flow
𝑑𝑑
0 = οΏ½ 𝜌𝜌𝜌𝜌𝜌𝜌 + 𝜌𝜌2 𝑉𝑉2 𝐴𝐴2 − 𝜌𝜌1 𝑉𝑉1 𝐴𝐴1 − (𝜌𝜌3 𝑉𝑉3 𝐴𝐴3 )
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
or,
𝑉𝑉2 𝐴𝐴2 = 𝑉𝑉1 𝐴𝐴1 + 𝑉𝑉�
3 𝐴𝐴3
= 𝑄𝑄3
𝑉𝑉1 𝐴𝐴1 + 𝑄𝑄3
3 πœ‹πœ‹ 0.05 2 /4 + (0.01)
∴ 𝑉𝑉2 =
=
= 4.13 m/s
𝐴𝐴2
πœ‹πœ‹ 0.07 2 /4
21
57:020 Fluids Mechanics Fall2013
Moving CV
22
57:020 Fluids Mechanics Fall2013
RTT for Moving CV
(i.e., relative velocity π‘‰π‘‰π‘Ÿπ‘Ÿ )
𝐷𝐷𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑
�𝑑𝑑𝑑𝑑
= οΏ½ π›½π›½πœŒπœŒπœŒπœŒπœŒπœŒ + οΏ½ π›½π›½πœŒπœŒπ‘‰π‘‰π‘Ÿπ‘Ÿ ⋅ 𝒏𝒏
𝐷𝐷𝐷𝐷
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
𝐢𝐢𝑆𝑆
23
57:020 Fluids Mechanics Fall2013
24
RTT for Moving and Deforming CV
𝑑𝑑𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑
οΏ½ 𝑑𝑑𝑑𝑑
= οΏ½ 𝛽𝛽𝛽𝛽𝛽𝛽𝛽𝛽 + οΏ½ 𝛽𝛽𝛽𝛽 𝑽𝑽𝒓𝒓 ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
𝐢𝐢𝑆𝑆
∗
Both CV and CS change their shape and location
with time
π‘½π‘½π‘Ÿπ‘Ÿ = 𝑽𝑽(𝒙𝒙, 𝑑𝑑) − 𝑽𝑽𝑆𝑆 (𝒙𝒙, 𝑑𝑑)
• 𝑉𝑉𝑆𝑆 (π‘₯π‘₯, 𝑑𝑑): Velocity of CS
• 𝑉𝑉(π‘₯π‘₯, 𝑑𝑑): Fluid velocity in the coordinate
system in which the 𝑉𝑉𝑠𝑠 is observed
• π‘‰π‘‰π‘Ÿπ‘Ÿ : Relative velocity of fluid seen by an
observer riding on the CV
*Ref) Fluid Mechanics by Frank M. White, McGraw Hill
57:020 Fluids Mechanics Fall2013
RTT Summary (1)
General RTT (for moving and deforming CV):
𝑑𝑑𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
𝑑𝑑
�𝑑𝑑𝑑𝑑
=
οΏ½ 𝛽𝛽𝛽𝛽𝛽𝛽𝛽𝛽 + οΏ½ π›½π›½π›½π›½π‘‰π‘‰π‘Ÿπ‘Ÿ ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑
𝑑𝑑𝑑𝑑 𝐢𝐢𝑉𝑉
𝐢𝐢𝑆𝑆
Special Cases:
1) Non-deforming (but moving) CV
𝑑𝑑𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
πœ•πœ•
�𝑑𝑑𝑑𝑑
=οΏ½
𝛽𝛽𝛽𝛽 𝑑𝑑𝑉𝑉 + οΏ½ π›½π›½π›½π›½π‘‰π‘‰π‘Ÿπ‘Ÿ ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑
πœ•πœ•πœ•πœ•
𝐢𝐢𝑉𝑉
𝐢𝐢𝑆𝑆
2) Fixed CV
𝑑𝑑𝐡𝐡𝑠𝑠𝑠𝑠𝑠𝑠
πœ•πœ•
�𝑑𝑑𝑑𝑑
=οΏ½
𝛽𝛽𝛽𝛽 𝑑𝑑𝑉𝑉 + οΏ½ 𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑
πœ•πœ•πœ•πœ•
𝐢𝐢𝑉𝑉
𝐢𝐢𝑆𝑆
3) Steady flow:
πœ•πœ•
=0
πœ•πœ•πœ•πœ•
4) Flux terms for uniform flow across discrete CS’s (steady or unsteady)
�𝑑𝑑𝑑𝑑 = οΏ½ π›½π›½π‘šπ‘šΜ‡
οΏ½ 𝛽𝛽𝛽𝛽𝑉𝑉 ⋅ 𝒏𝒏
𝐢𝐢𝑆𝑆
π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
− οΏ½ π›½π›½π‘šπ‘šΜ‡
𝑖𝑖𝑖𝑖
25
57:020 Fluids Mechanics Fall2013
RTT Summary (2)
For fixed CV’s:
Parameter (𝐡𝐡)
𝛽𝛽 = 𝐡𝐡/π‘šπ‘š
Mass (π‘šπ‘š)
1
0=
𝑉𝑉
� 𝐹𝐹 =
𝑒𝑒
𝑄𝑄̇ − π‘Šπ‘ŠΜ‡ =
Momentum
(π‘šπ‘šπ‘‰π‘‰)
Energy (𝐸𝐸)
RTT
𝑑𝑑
�𝑑𝑑𝐴𝐴
οΏ½ πœŒπœŒπœŒπœŒπ‘‰π‘‰ + οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
𝐢𝐢𝐢𝐢
𝑑𝑑
�𝑑𝑑𝐴𝐴
οΏ½ π‘‰π‘‰πœŒπœŒπœŒπœŒπ‘‰π‘‰ + οΏ½ π‘‰π‘‰πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
𝐢𝐢𝐢𝐢
𝑑𝑑
�𝑑𝑑𝐴𝐴
οΏ½ 𝑒𝑒𝑒𝑒𝑒𝑒𝑉𝑉 + οΏ½ 𝑒𝑒𝑒𝑒𝑉𝑉 ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
𝐢𝐢𝐢𝐢
Remark
Continuity eq.
(Ch. 5.1)
Linear momentum eq.
(Ch. 5.2)
Energy eq.
(Ch. 5.3)
26
57:020 Fluids Mechanics Fall2013
Continuity Equation (Ch. 5.1)
RTT with 𝐡𝐡 = mass and 𝛽𝛽 = 1,
or
𝐷𝐷𝑀𝑀𝑠𝑠𝑠𝑠𝑠𝑠
0=
𝐷𝐷𝐷𝐷
mass conservatoin
𝑑𝑑
�𝑑𝑑𝐴𝐴
= οΏ½ πœŒπœŒπœŒπœŒπ‘‰π‘‰ + οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
𝐢𝐢𝐢𝐢
�𝑑𝑑𝐴𝐴
οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝐢𝐢𝐢𝐢
Net rate of outflow
of mass across CS
=
−
𝑑𝑑
οΏ½ πœŒπœŒπœŒπœŒπ‘‰π‘‰
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
Rate of decrease of
mass within CV
Note: Incompressible fluid (𝜌𝜌 = constant)
𝑑𝑑
�𝑑𝑑𝐴𝐴 = − οΏ½ 𝑑𝑑𝑉𝑉
οΏ½ 𝑉𝑉 ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
𝐢𝐢𝐢𝐢
(Conservation of volume)
27
57:020 Fluids Mechanics Fall2013
Simplifications
1. Steady flow
�𝑑𝑑𝐴𝐴 = 0
οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝐢𝐢𝐢𝐢
2. If 𝑉𝑉 = constant over discrete CS’s (i.e., one-dimensional flow)
�𝑑𝑑𝑑𝑑 = οΏ½ 𝜌𝜌𝜌𝜌𝜌𝜌 − οΏ½ πœŒπœŒπ‘‰π‘‰π΄π΄
οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝐢𝐢𝑆𝑆
π‘œπ‘œπ‘’π‘’π‘’π‘’
3. Steady one-dimensional flow in a conduit
or
For 𝜌𝜌 = constant
𝜌𝜌𝜌𝜌𝜌𝜌
π‘œπ‘œπ‘œπ‘œπ‘œπ‘œ
− 𝜌𝜌𝜌𝜌𝜌𝜌
𝑖𝑖𝑖𝑖
𝑖𝑖𝑖𝑖
=0
𝜌𝜌2 𝑉𝑉2 𝐴𝐴2 − 𝜌𝜌1 𝑉𝑉1 𝐴𝐴1 = 0
𝑉𝑉1 𝐴𝐴1 = 𝑉𝑉2 𝐴𝐴2 (or 𝑄𝑄1 = 𝑄𝑄2 )
28
57:020 Fluids Mechanics Fall2013
Some useful definitions
Mass flux
π‘šπ‘šΜ‡ = οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝑑𝑑𝑑𝑑
𝐴𝐴
Volume flux
�𝑑𝑑𝑑𝑑)
(Note: 𝑉𝑉 ⋅ 𝑑𝑑𝑑𝑑 = 𝑉𝑉 ⋅ 𝒏𝒏
𝑄𝑄 = οΏ½ 𝑉𝑉 ⋅ 𝑑𝑑𝐴𝐴
𝐴𝐴
Average velocity
𝐴𝐴̅ =
Average density
πœŒπœŒΜ… =
𝑄𝑄 1
= οΏ½ 𝑉𝑉 ⋅ 𝑑𝑑𝐴𝐴
𝐴𝐴 𝐴𝐴 𝐴𝐴
1
� 𝜌𝜌𝜌𝜌𝜌𝜌
𝐴𝐴 𝐴𝐴
Note: π‘šπ‘šΜ‡ ≠ πœŒπœŒΜ… 𝑄𝑄 unless 𝜌𝜌 = constant
29
57:020 Fluids Mechanics Fall2013
Example 4
Estimate the time required to fill with
water a cone-shaped container 5 ft hight
and 5 ft across at the top if the filling rate
is 20 gal/min.
Apply the conservation of mass (𝛽𝛽 = 1)
𝑑𝑑
�𝑑𝑑𝐴𝐴
0 = οΏ½ πœŒπœŒπœŒπœŒπ‘‰π‘‰ + οΏ½ πœŒπœŒπ‘‰π‘‰ ⋅ 𝒏𝒏
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
𝐢𝐢𝐢𝐢
For incompressible fluid (i.e., 𝜌𝜌 = constant) and one inlet,
0=
𝑑𝑑
οΏ½ 𝑑𝑑𝑉𝑉 − 𝑉𝑉𝑉𝑉
𝑑𝑑𝑑𝑑 𝐢𝐢𝐢𝐢
=𝑉𝑉
𝑖𝑖𝑖𝑖
=𝑄𝑄𝑖𝑖𝑖𝑖
30
57:020 Fluids Mechanics Fall2013
Example 4 – Contd.
Volume of the cone at time t,
πœ‹πœ‹π·π·2
𝑉𝑉 𝑑𝑑 =
β„Ž 𝑑𝑑
12
Flow rate at the inlet,
gal
𝑄𝑄 = 20
min
The continuity eq. becomes
πœ‹πœ‹π·π·2 𝑑𝑑𝑑
⋅
= 𝑄𝑄
12 𝑑𝑑𝑑𝑑
in3
in3
231
οΏ½ 1,728 3 = 2.674 ft 3 /min
gal
ft
or
𝑑𝑑𝑑 12𝑄𝑄
=
𝑑𝑑𝑑𝑑 πœ‹πœ‹π·π·2
31
57:020 Fluids Mechanics Fall2013
Example 4 – Contd.
Solve for β„Ž(𝑑𝑑),
𝑑𝑑
12𝑄𝑄
12𝑄𝑄 ⋅ 𝑑𝑑
β„Ž 𝑑𝑑 = οΏ½
𝑑𝑑𝑑𝑑 =
2
πœ‹πœ‹π·π·
πœ‹πœ‹π·π·2
0
Thus, the time for β„Ž = 5 ft is
πœ‹πœ‹π·π·2 β„Ž
πœ‹πœ‹ 5 ft 2 (5 ft)
𝑑𝑑 =
=
= 12.2 min
12𝑄𝑄
(12)(2.674 ft 3 /min)
32
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