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‫الرح‬ ‫الرحمن‬ ‫هللا‬ ‫بسم‬
‫يم‬
(
)
‫صدق‬
‫هللا‬
‫العلي‬
‫العظيم‬
(
‫البقرة‬
/
32
)
Applications of Differential Equations
‫المعادالت‬ ‫تطبيقات‬
‫التفاضلية‬
An example is the application of partial
differential equations in fluid mechanics
‫ف‬ ‫الجزئية‬ ‫التفاضلية‬ ‫المعادالت‬ ‫تطبيقات‬ ‫ذلك‬ ‫على‬ ‫مثال‬
‫ي‬
‫الموائع‬ ‫ميكانيكا‬
BY
Mohammed R. Salman
Solids Gasses
Resist a shear stress
Science of flow (rheological)
Hydraulics Hydrodynamics
Experimental studies theoretical studies
Fluid Mechanics
Introduction
liquids
Matter
Peristalsis is defined as a wave of relaxation contraction imparted to the walls of
a flexible conduit effecting the pumping of enclosed material.
Peristaltic phenomenon
Practical
applications
Physiology
Bio-
mechanical
Examples
Examples of Peristalsis
Transport
Types of Fluids
Newtonian Fluids Non-Newtonian Fluids
Water
Blood
Silicon
ketchup
molasses
n
du
= + B
dy
 
 
 
 
Alcohol
Gasoline
The Flexible Channels
Co-axial pipes
Curved pipes
Straight pipes
Tapered pipes
Symmetric motion Anti-symmetric motion
uniform Non-uniform
0 ≤ ∅ ≤ 𝜋
Elementary concepts and basic definitions
Fluid mechanics
Is that branch of applied mathematics which deal with the behavior of fluid at rest
and in motion.
 Statics  Kinematic  Dynamic
Relation between the
stress and the rateof strain
Classification of fluid
0



t
p
0
V
t



Effect of convective conditions in a radiative peristaltic flow of
pseudoplastic nanofluid through a porous medium in a tapered an
inclined asymmetric channel
‫للمائع‬ ‫الشعاعي‬ ‫الجريان‬ ‫على‬ ‫الحدودية‬ ‫الشروط‬ ‫تأثير‬
‫النانوي‬
‫خ‬ ‫الكاذب‬
‫الل‬
‫متماثلة‬ ‫غير‬ ‫مائلة‬ ‫مستدقة‬ ‫قناة‬ ‫في‬ ‫مسامي‬ ‫وسط‬
d
d
T0
b
2
b
1
H
2
H
1
T1
X
Y
𝑌 = 𝐻2 𝑋, 𝑡 = 𝑑 + 𝑚𝑋 + 𝑏2 𝑆𝑖𝑛
2𝜋
𝜆
𝑋 − 𝑐𝑡
𝑌 = 𝐻1 𝑋, 𝑡 = −𝑑 − 𝑚𝑋 − 𝑏1 𝑆𝑖𝑛
2𝜋
𝜆
𝑋 − 𝑐𝑡 + 𝜙
Calculation of Lorentz force
𝑉 × 𝐵 =
𝑖 𝑗 𝑘
𝑢 𝑣 0
0 𝐵0 0
= 𝐵0𝑢𝑘
𝐽 = 𝜎 𝑉 × 𝐵 = 𝜎𝐵0𝑢 𝑘
𝐽 × 𝐵 =
𝑖 𝑗 𝑘
0 0 𝜎𝐵0𝑢
0 𝐵0 0
= −𝜎𝐵0
2
𝑢 𝑖 .
Both walls move towards outward or inward simultaneously and further
𝑏1,𝑏2,𝑑 and 𝜙 satisfy the following condition at the inlet of divergent channel
𝑏1
2
+ 𝑏2
2
+ 2𝑏1𝑏2 𝐶𝑜𝑠(𝜙) ≤ 𝑑1 + 𝑑2
2
Constitutive Equations
𝑺 + 𝜆1
𝐷𝑺
𝐷𝑡
+
1
2
𝜆1 − 𝜇1 𝐴1𝑺 + 𝑺𝐴1 = 𝜇𝐴1
𝐴1 = 𝛻𝑉 + 𝛻𝑉
𝑇
𝑑𝑺 𝑑𝑡 = 𝜕𝑺 𝜕𝑡 + 𝑽. 𝛻𝑺
𝐷𝑺
𝐷𝑡
= 𝑑𝑺 𝑑𝑡 − 𝛻𝑉 𝑺 − 𝑺 𝛻𝑉
𝑇
𝐷𝑺
𝐷𝑡
= 𝜕𝑺 𝜕𝑡 + 𝑽. 𝛻𝑺 − 𝛻𝑉 𝑺 − 𝑺 𝛻𝑉
𝑇
𝑺 =
𝑆𝑋𝑋 𝑆𝑋𝑌
𝑆𝑌𝑋 𝑆𝑌𝑌
=
𝑎11 𝑎12
𝑎21 𝑎22
, 𝐴1 =
2
𝜕𝑈
𝜕𝑋
𝜕𝑈
𝜕𝑌
+
𝜕𝑉
𝜕𝑋
𝜕𝑉
𝜕𝑋
+
𝜕𝑈
𝜕𝑌
2
𝜕𝑉
𝜕𝑌
The Components of Stress Tensor
𝑆𝑋𝑋 + 𝜆1
𝜕
𝜕𝑡
+ 𝑈
𝜕
𝜕𝑋
+ 𝑉
𝜕
𝜕𝑌
𝑆𝑋𝑋 − 2𝑆𝑋𝑋
𝜕𝑈
𝜕𝑋
− 2𝑆𝑋𝑌
𝜕𝑈
𝜕𝑌
+
1
2
𝜆1 − 𝜇1 4𝑆𝑋𝑋
𝜕𝑈
𝜕𝑋
+ 2𝑆𝑋𝑌
𝜕𝑈
𝜕𝑌
+
𝜕𝑉
𝜕𝑋
= 2𝜇
𝜕𝑈
𝜕𝑋
……(1)
𝑆𝑋𝑌 + 𝜆1
𝜕
𝜕𝑡
+ 𝑈
𝜕
𝜕𝑋
+ 𝑉
𝜕
𝜕𝑌
𝑆𝑋𝑌 − 𝑆𝑋𝑋
𝜕𝑉
𝜕𝑋
− 𝑆𝑌𝑌
𝜕𝑈
𝜕𝑌
+
1
2
𝜆1 − 𝜇1 𝑆𝑋𝑋 + 𝑆𝑌𝑌
𝜕𝑈
𝜕𝑌
+
𝜕𝑉
𝜕𝑋
= 𝜇
𝜕𝑈
𝜕𝑌
+
𝜕𝑉
𝜕𝑋
…….(2)
𝑆𝑌𝑌 + 𝜆1
𝜕
𝜕𝑡
+ 𝑈
𝜕
𝜕𝑋
+ 𝑉
𝜕
𝜕𝑌
𝑆𝑌𝑌 − 2𝑆𝑌𝑋
𝜕𝑉
𝜕𝑋
− 2𝑆𝑌𝑌
𝜕𝑉
𝜕𝑌
+
1
2
𝜆1 − 𝜇1 2𝑆𝑋𝑌
𝜕𝑈
𝜕𝑌
+
𝜕𝑉
𝜕𝑋
+ 4𝑆𝑌𝑌
𝜕𝑉
𝜕𝑌
= 2𝜇
𝜕𝑉
𝜕𝑌
……(3)
Governing Equations
𝜕𝑈
𝜕𝑋
+
𝜕𝑉
𝜕𝑌
= 0
…(4)
𝜌𝑓
𝜕𝑈
𝜕𝑡
+ 𝑈
𝜕𝑈
𝜕𝑋
+ 𝑉
𝜕𝑈
𝜕𝑌
= −
𝜕𝑃
𝜕𝑋
+
𝜕
𝜕𝑋
𝑆𝑋𝑋 +
𝜕
𝜕𝑌
𝑆𝑋𝑌 − 𝝈𝐵𝟎
2
𝑈 −
𝜇
𝐾0
𝑈 +𝜌𝑓 𝑔 𝑠𝑖𝑛𝛼
𝜌𝑓
𝜕𝑉
𝜕𝑡
+ 𝑈
𝜕𝑉
𝜕𝑋
+ 𝑉
𝜕𝑉
𝜕𝑌
= −
𝜕𝑃
𝜕𝑌
+
𝜕
𝜕𝑋
𝑆𝑌𝑋 +
𝜕
𝜕𝑌
𝑆𝑌𝑌 −
𝜇
𝐾0
𝑉 −𝜌𝑓 𝑔 𝑐𝑜𝑠𝛼 …(6)
(𝜌𝑐)𝑓
𝜕𝑇
𝜕𝑡
+ 𝑈
𝜕𝑇
𝜕𝑋
+ 𝑉
𝜕𝑇
𝜕𝑌
= 𝜅
𝜕2𝑇
𝜕𝑋2 +
𝜕2𝑇
𝜕𝑌2 + (𝜌𝑐)𝑝
𝐷𝑇
𝑇𝑚
𝜕𝑇
𝜕𝑋
2
+
𝜕𝑇
𝜕𝑌
2
…(7)
…(5)
Fixed frame (𝑿,𝒀,𝒕) Wave frame 𝒙,𝒚
𝑥 = 𝑋 − 𝑐𝑡 ,𝑦 = 𝑌,𝑢 𝑥,𝑦 = 𝑈 𝑋,𝑌,𝑡 − 𝑐 ,𝑣 𝑥,𝑦 = 𝑉 𝑋,𝑌,𝑡 , 𝑝 𝑥,𝑦 = 𝑃 𝑋,𝑌,𝑡
The coordinates and velocities in the two frames are
related by
Dimensionless Analysis
𝑥 =
𝑥
𝜆
, 𝑦 =
𝑦
𝑑
, 𝑡 =
𝑐𝑡
𝜆
, 𝑢 =
𝑢
𝑐
, 𝑣 =
𝑣
𝑐
, 𝛿 =
𝑑
𝜆
, ℎ1 =
𝐻1
𝑑
, ℎ2 =
𝐻2
𝑑
, 𝜃 =
𝑇 − 𝑇°
𝑇1 − 𝑇°
,
𝑝 =
𝑑2𝑝
𝜆𝜇𝑐
, 𝑆𝑖𝑗 =
𝑑
𝑐𝜇
𝑆𝑖𝑗 , 𝜆1
∗
=
𝜆1𝑐
𝑑
, 𝜇1
∗
=
𝜇1𝑐
𝑑
, 𝐾 =
𝐾0
𝑑2
, 𝑅𝑒 =
𝜌𝑓𝑐𝑑
𝜇
, 𝑎 =
𝑏1
𝑑
, 𝑏 =
𝑏2
𝑑
,
m =
mλ
d
, Pr =
μcf
κ
, Nt =
τDT(T1 − T0)
Tm𝓋
, M =
σ
μ
dB0, u =
𝜕ψ
𝜕y
, v = −δ
𝜕ψ
𝜕x
𝜕𝑝
𝜕𝑥
=
𝜕
𝜕𝑦
𝑆𝑥𝑦 − 𝑀2 +
1
𝐾
𝜕𝜓
𝜕𝑦
+ 1
𝜕𝑝
𝜕𝑦
= 0
𝜕2
𝜃
𝜕𝑦2
+ 𝑃𝑟𝑁𝑡
𝜕𝜃
𝜕𝑦
2
= 0
long-wavelength approximation i.e.(𝜹 ≪ 𝟏) and the low Reynolds
number i.e. (𝑹𝒆 → 𝟎).
(8)
(9)
(10)
𝑆𝑥𝑥 = 𝜆1 + 𝜇1 𝑆𝑥𝑦
𝜕2𝜓
𝜕𝑦2
(11)
𝑆𝑥𝑦 +
1
2
𝜆1 − 𝜇1 𝑆𝑥𝑥 + 𝑆𝑦𝑦
𝜕2𝜓
𝜕𝑦2 − 𝜆1𝑆𝑦𝑦
𝜕2𝜓
𝜕𝑦2 =
𝜕2𝜓
𝜕𝑦2 (12)
𝑆𝑦𝑦 = − 𝜆1 − 𝜇1 𝑆𝑥𝑦
𝜕2
𝜓
𝜕𝑦2
(13)
𝜕𝑝
𝜕𝑥
=
𝜕3𝜓
𝜕𝑦3
+ 𝜉
𝜕
𝜕𝑦
𝜕2𝜓
𝜕𝑦2
3
+ 𝜉2
𝜕
𝜕𝑦
𝜕2𝜓
𝜕𝑦2
4
− 𝑁2
𝜕𝜓
𝜕𝑦
+ 1
𝜕4
𝜓
𝜕𝑦4 + 3𝜉
𝜕2
𝜓
𝜕𝑦2
2
𝜕4
𝜓
𝜕𝑦4 + 2
𝜕3
𝜓
𝜕𝑦3
2
𝜕2
𝜓
𝜕𝑦2 − 𝑁2
𝜕2
𝜓
𝜕𝑦2 = 0
After using binomial expansion for small pseudoplastic fluid parameter
𝜉 ,where 𝜉 = (𝜇1
2
− 𝜆1
2
) and 𝑁2 = 𝑀2 +
1
𝐾
we get:
(14)
(15)
Perturbed System and Perturbation Solutions:
In order to solve the present problem, we expand the flow quantities
in a power series of 𝜉 𝑎𝑛𝑑 𝑃𝑟
𝑃 = 𝑃0 +𝜉𝑃1 + 𝜉2𝑃2 + ⋯
𝜓 = 𝜓0 + 𝜉𝜓1 + 𝜉2
𝜓2 + ⋯
𝐹 = 𝐹0 +𝜉𝐹1 + 𝜉2
𝐹2 + ⋯
𝜃 = 𝜃0 +𝑃𝑟𝜃1 + 𝑃𝑟2
𝜃2 + ⋯
Zeroth- Order System
𝜕4𝜓0
𝜕𝑦4
− 𝑁2
𝜕2𝜓0
𝜕𝑦2
= 0
𝜕𝑝0
𝜕𝑥
=
𝜕3𝜓0
𝜕𝑦3 − 𝑁2
𝜕𝜓0
𝜕𝑦
+ 1 = 0
𝜕2𝜃0
𝜕𝑦2
= 0
With corresponding convective boundary conditions
𝜓0 = −
𝐹0
2
,
𝜕𝜓0
𝜕𝑦
= 0 , 𝜃0 = 0, 𝑎𝑡 𝑦 = ℎ1
𝜓0 =
𝐹0
2
,
𝜕𝜓0
𝜕𝑦
= 0 , 𝜃0 = 1 , 𝑎𝑡 𝑦 = ℎ2
First- Order System
𝜕4𝜓1
𝜕𝑦4 + 3
𝜕4𝜓0
𝜕𝑦4
𝜕2𝜓0
𝜕𝑦2
2
+ 6
𝜕3𝜓0
𝜕𝑦3
2
𝜕2𝜓0
𝜕𝑦2 − 𝑁2
𝜕2𝜓1
𝜕𝑦2 = 0
𝜕𝑝1
𝜕𝑥
−
𝜕3𝜓1
𝜕𝑦3
− 3
𝜕3𝜓0
𝜕𝑦3
𝜕2𝜓0
𝜕𝑦2
2
+ 𝑁2
𝜕𝜓1
𝜕𝑦
= 0
𝜕2𝜃1
𝜕𝑦2
+ 𝑁𝑡
𝜕𝜃0
𝜕𝑦
2
= 0
𝜓1 = −
𝐹1
2
,
𝜕𝜓1
𝜕𝑦
= 0, 𝜃1 = 0 𝑎𝑡 𝑦 = ℎ1
𝜓1 =
𝐹1
2
,
𝜕𝜓1
𝜕𝑦
= 0, 𝜃1 = 0 𝑎𝑡 𝑦 = ℎ2
With corresponding convective boundary conditions
GRAPHS
Velocity profile
Temperature distribution
Pressure rise
Heat transfer coefficient
Trapping phenomenon
m Q
ξ
M K
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Applications of Differential Equations Fluid Mechanics

  • 1. ‫الرح‬ ‫الرحمن‬ ‫هللا‬ ‫بسم‬ ‫يم‬ ( ) ‫صدق‬ ‫هللا‬ ‫العلي‬ ‫العظيم‬ ( ‫البقرة‬ / 32 )
  • 2. Applications of Differential Equations ‫المعادالت‬ ‫تطبيقات‬ ‫التفاضلية‬ An example is the application of partial differential equations in fluid mechanics ‫ف‬ ‫الجزئية‬ ‫التفاضلية‬ ‫المعادالت‬ ‫تطبيقات‬ ‫ذلك‬ ‫على‬ ‫مثال‬ ‫ي‬ ‫الموائع‬ ‫ميكانيكا‬ BY Mohammed R. Salman
  • 3. Solids Gasses Resist a shear stress Science of flow (rheological) Hydraulics Hydrodynamics Experimental studies theoretical studies Fluid Mechanics Introduction liquids Matter
  • 4. Peristalsis is defined as a wave of relaxation contraction imparted to the walls of a flexible conduit effecting the pumping of enclosed material. Peristaltic phenomenon Practical applications Physiology Bio- mechanical Examples
  • 6. Types of Fluids Newtonian Fluids Non-Newtonian Fluids Water Blood Silicon ketchup molasses n du = + B dy         Alcohol Gasoline
  • 7. The Flexible Channels Co-axial pipes Curved pipes Straight pipes Tapered pipes Symmetric motion Anti-symmetric motion uniform Non-uniform 0 ≤ ∅ ≤ 𝜋
  • 8. Elementary concepts and basic definitions Fluid mechanics Is that branch of applied mathematics which deal with the behavior of fluid at rest and in motion.  Statics  Kinematic  Dynamic Relation between the stress and the rateof strain Classification of fluid
  • 10. Effect of convective conditions in a radiative peristaltic flow of pseudoplastic nanofluid through a porous medium in a tapered an inclined asymmetric channel ‫للمائع‬ ‫الشعاعي‬ ‫الجريان‬ ‫على‬ ‫الحدودية‬ ‫الشروط‬ ‫تأثير‬ ‫النانوي‬ ‫خ‬ ‫الكاذب‬ ‫الل‬ ‫متماثلة‬ ‫غير‬ ‫مائلة‬ ‫مستدقة‬ ‫قناة‬ ‫في‬ ‫مسامي‬ ‫وسط‬ d d T0 b 2 b 1 H 2 H 1 T1 X Y 𝑌 = 𝐻2 𝑋, 𝑡 = 𝑑 + 𝑚𝑋 + 𝑏2 𝑆𝑖𝑛 2𝜋 𝜆 𝑋 − 𝑐𝑡 𝑌 = 𝐻1 𝑋, 𝑡 = −𝑑 − 𝑚𝑋 − 𝑏1 𝑆𝑖𝑛 2𝜋 𝜆 𝑋 − 𝑐𝑡 + 𝜙
  • 11. Calculation of Lorentz force 𝑉 × 𝐵 = 𝑖 𝑗 𝑘 𝑢 𝑣 0 0 𝐵0 0 = 𝐵0𝑢𝑘 𝐽 = 𝜎 𝑉 × 𝐵 = 𝜎𝐵0𝑢 𝑘 𝐽 × 𝐵 = 𝑖 𝑗 𝑘 0 0 𝜎𝐵0𝑢 0 𝐵0 0 = −𝜎𝐵0 2 𝑢 𝑖 . Both walls move towards outward or inward simultaneously and further 𝑏1,𝑏2,𝑑 and 𝜙 satisfy the following condition at the inlet of divergent channel 𝑏1 2 + 𝑏2 2 + 2𝑏1𝑏2 𝐶𝑜𝑠(𝜙) ≤ 𝑑1 + 𝑑2 2
  • 12. Constitutive Equations 𝑺 + 𝜆1 𝐷𝑺 𝐷𝑡 + 1 2 𝜆1 − 𝜇1 𝐴1𝑺 + 𝑺𝐴1 = 𝜇𝐴1 𝐴1 = 𝛻𝑉 + 𝛻𝑉 𝑇 𝑑𝑺 𝑑𝑡 = 𝜕𝑺 𝜕𝑡 + 𝑽. 𝛻𝑺 𝐷𝑺 𝐷𝑡 = 𝑑𝑺 𝑑𝑡 − 𝛻𝑉 𝑺 − 𝑺 𝛻𝑉 𝑇 𝐷𝑺 𝐷𝑡 = 𝜕𝑺 𝜕𝑡 + 𝑽. 𝛻𝑺 − 𝛻𝑉 𝑺 − 𝑺 𝛻𝑉 𝑇 𝑺 = 𝑆𝑋𝑋 𝑆𝑋𝑌 𝑆𝑌𝑋 𝑆𝑌𝑌 = 𝑎11 𝑎12 𝑎21 𝑎22 , 𝐴1 = 2 𝜕𝑈 𝜕𝑋 𝜕𝑈 𝜕𝑌 + 𝜕𝑉 𝜕𝑋 𝜕𝑉 𝜕𝑋 + 𝜕𝑈 𝜕𝑌 2 𝜕𝑉 𝜕𝑌
  • 13. The Components of Stress Tensor 𝑆𝑋𝑋 + 𝜆1 𝜕 𝜕𝑡 + 𝑈 𝜕 𝜕𝑋 + 𝑉 𝜕 𝜕𝑌 𝑆𝑋𝑋 − 2𝑆𝑋𝑋 𝜕𝑈 𝜕𝑋 − 2𝑆𝑋𝑌 𝜕𝑈 𝜕𝑌 + 1 2 𝜆1 − 𝜇1 4𝑆𝑋𝑋 𝜕𝑈 𝜕𝑋 + 2𝑆𝑋𝑌 𝜕𝑈 𝜕𝑌 + 𝜕𝑉 𝜕𝑋 = 2𝜇 𝜕𝑈 𝜕𝑋 ……(1) 𝑆𝑋𝑌 + 𝜆1 𝜕 𝜕𝑡 + 𝑈 𝜕 𝜕𝑋 + 𝑉 𝜕 𝜕𝑌 𝑆𝑋𝑌 − 𝑆𝑋𝑋 𝜕𝑉 𝜕𝑋 − 𝑆𝑌𝑌 𝜕𝑈 𝜕𝑌 + 1 2 𝜆1 − 𝜇1 𝑆𝑋𝑋 + 𝑆𝑌𝑌 𝜕𝑈 𝜕𝑌 + 𝜕𝑉 𝜕𝑋 = 𝜇 𝜕𝑈 𝜕𝑌 + 𝜕𝑉 𝜕𝑋 …….(2) 𝑆𝑌𝑌 + 𝜆1 𝜕 𝜕𝑡 + 𝑈 𝜕 𝜕𝑋 + 𝑉 𝜕 𝜕𝑌 𝑆𝑌𝑌 − 2𝑆𝑌𝑋 𝜕𝑉 𝜕𝑋 − 2𝑆𝑌𝑌 𝜕𝑉 𝜕𝑌 + 1 2 𝜆1 − 𝜇1 2𝑆𝑋𝑌 𝜕𝑈 𝜕𝑌 + 𝜕𝑉 𝜕𝑋 + 4𝑆𝑌𝑌 𝜕𝑉 𝜕𝑌 = 2𝜇 𝜕𝑉 𝜕𝑌 ……(3)
  • 14. Governing Equations 𝜕𝑈 𝜕𝑋 + 𝜕𝑉 𝜕𝑌 = 0 …(4) 𝜌𝑓 𝜕𝑈 𝜕𝑡 + 𝑈 𝜕𝑈 𝜕𝑋 + 𝑉 𝜕𝑈 𝜕𝑌 = − 𝜕𝑃 𝜕𝑋 + 𝜕 𝜕𝑋 𝑆𝑋𝑋 + 𝜕 𝜕𝑌 𝑆𝑋𝑌 − 𝝈𝐵𝟎 2 𝑈 − 𝜇 𝐾0 𝑈 +𝜌𝑓 𝑔 𝑠𝑖𝑛𝛼 𝜌𝑓 𝜕𝑉 𝜕𝑡 + 𝑈 𝜕𝑉 𝜕𝑋 + 𝑉 𝜕𝑉 𝜕𝑌 = − 𝜕𝑃 𝜕𝑌 + 𝜕 𝜕𝑋 𝑆𝑌𝑋 + 𝜕 𝜕𝑌 𝑆𝑌𝑌 − 𝜇 𝐾0 𝑉 −𝜌𝑓 𝑔 𝑐𝑜𝑠𝛼 …(6) (𝜌𝑐)𝑓 𝜕𝑇 𝜕𝑡 + 𝑈 𝜕𝑇 𝜕𝑋 + 𝑉 𝜕𝑇 𝜕𝑌 = 𝜅 𝜕2𝑇 𝜕𝑋2 + 𝜕2𝑇 𝜕𝑌2 + (𝜌𝑐)𝑝 𝐷𝑇 𝑇𝑚 𝜕𝑇 𝜕𝑋 2 + 𝜕𝑇 𝜕𝑌 2 …(7) …(5)
  • 15. Fixed frame (𝑿,𝒀,𝒕) Wave frame 𝒙,𝒚 𝑥 = 𝑋 − 𝑐𝑡 ,𝑦 = 𝑌,𝑢 𝑥,𝑦 = 𝑈 𝑋,𝑌,𝑡 − 𝑐 ,𝑣 𝑥,𝑦 = 𝑉 𝑋,𝑌,𝑡 , 𝑝 𝑥,𝑦 = 𝑃 𝑋,𝑌,𝑡 The coordinates and velocities in the two frames are related by Dimensionless Analysis 𝑥 = 𝑥 𝜆 , 𝑦 = 𝑦 𝑑 , 𝑡 = 𝑐𝑡 𝜆 , 𝑢 = 𝑢 𝑐 , 𝑣 = 𝑣 𝑐 , 𝛿 = 𝑑 𝜆 , ℎ1 = 𝐻1 𝑑 , ℎ2 = 𝐻2 𝑑 , 𝜃 = 𝑇 − 𝑇° 𝑇1 − 𝑇° , 𝑝 = 𝑑2𝑝 𝜆𝜇𝑐 , 𝑆𝑖𝑗 = 𝑑 𝑐𝜇 𝑆𝑖𝑗 , 𝜆1 ∗ = 𝜆1𝑐 𝑑 , 𝜇1 ∗ = 𝜇1𝑐 𝑑 , 𝐾 = 𝐾0 𝑑2 , 𝑅𝑒 = 𝜌𝑓𝑐𝑑 𝜇 , 𝑎 = 𝑏1 𝑑 , 𝑏 = 𝑏2 𝑑 , m = mλ d , Pr = μcf κ , Nt = τDT(T1 − T0) Tm𝓋 , M = σ μ dB0, u = 𝜕ψ 𝜕y , v = −δ 𝜕ψ 𝜕x
  • 16. 𝜕𝑝 𝜕𝑥 = 𝜕 𝜕𝑦 𝑆𝑥𝑦 − 𝑀2 + 1 𝐾 𝜕𝜓 𝜕𝑦 + 1 𝜕𝑝 𝜕𝑦 = 0 𝜕2 𝜃 𝜕𝑦2 + 𝑃𝑟𝑁𝑡 𝜕𝜃 𝜕𝑦 2 = 0 long-wavelength approximation i.e.(𝜹 ≪ 𝟏) and the low Reynolds number i.e. (𝑹𝒆 → 𝟎). (8) (9) (10) 𝑆𝑥𝑥 = 𝜆1 + 𝜇1 𝑆𝑥𝑦 𝜕2𝜓 𝜕𝑦2 (11) 𝑆𝑥𝑦 + 1 2 𝜆1 − 𝜇1 𝑆𝑥𝑥 + 𝑆𝑦𝑦 𝜕2𝜓 𝜕𝑦2 − 𝜆1𝑆𝑦𝑦 𝜕2𝜓 𝜕𝑦2 = 𝜕2𝜓 𝜕𝑦2 (12) 𝑆𝑦𝑦 = − 𝜆1 − 𝜇1 𝑆𝑥𝑦 𝜕2 𝜓 𝜕𝑦2 (13)
  • 17. 𝜕𝑝 𝜕𝑥 = 𝜕3𝜓 𝜕𝑦3 + 𝜉 𝜕 𝜕𝑦 𝜕2𝜓 𝜕𝑦2 3 + 𝜉2 𝜕 𝜕𝑦 𝜕2𝜓 𝜕𝑦2 4 − 𝑁2 𝜕𝜓 𝜕𝑦 + 1 𝜕4 𝜓 𝜕𝑦4 + 3𝜉 𝜕2 𝜓 𝜕𝑦2 2 𝜕4 𝜓 𝜕𝑦4 + 2 𝜕3 𝜓 𝜕𝑦3 2 𝜕2 𝜓 𝜕𝑦2 − 𝑁2 𝜕2 𝜓 𝜕𝑦2 = 0 After using binomial expansion for small pseudoplastic fluid parameter 𝜉 ,where 𝜉 = (𝜇1 2 − 𝜆1 2 ) and 𝑁2 = 𝑀2 + 1 𝐾 we get: (14) (15) Perturbed System and Perturbation Solutions: In order to solve the present problem, we expand the flow quantities in a power series of 𝜉 𝑎𝑛𝑑 𝑃𝑟 𝑃 = 𝑃0 +𝜉𝑃1 + 𝜉2𝑃2 + ⋯ 𝜓 = 𝜓0 + 𝜉𝜓1 + 𝜉2 𝜓2 + ⋯ 𝐹 = 𝐹0 +𝜉𝐹1 + 𝜉2 𝐹2 + ⋯ 𝜃 = 𝜃0 +𝑃𝑟𝜃1 + 𝑃𝑟2 𝜃2 + ⋯
  • 18. Zeroth- Order System 𝜕4𝜓0 𝜕𝑦4 − 𝑁2 𝜕2𝜓0 𝜕𝑦2 = 0 𝜕𝑝0 𝜕𝑥 = 𝜕3𝜓0 𝜕𝑦3 − 𝑁2 𝜕𝜓0 𝜕𝑦 + 1 = 0 𝜕2𝜃0 𝜕𝑦2 = 0 With corresponding convective boundary conditions 𝜓0 = − 𝐹0 2 , 𝜕𝜓0 𝜕𝑦 = 0 , 𝜃0 = 0, 𝑎𝑡 𝑦 = ℎ1 𝜓0 = 𝐹0 2 , 𝜕𝜓0 𝜕𝑦 = 0 , 𝜃0 = 1 , 𝑎𝑡 𝑦 = ℎ2
  • 19. First- Order System 𝜕4𝜓1 𝜕𝑦4 + 3 𝜕4𝜓0 𝜕𝑦4 𝜕2𝜓0 𝜕𝑦2 2 + 6 𝜕3𝜓0 𝜕𝑦3 2 𝜕2𝜓0 𝜕𝑦2 − 𝑁2 𝜕2𝜓1 𝜕𝑦2 = 0 𝜕𝑝1 𝜕𝑥 − 𝜕3𝜓1 𝜕𝑦3 − 3 𝜕3𝜓0 𝜕𝑦3 𝜕2𝜓0 𝜕𝑦2 2 + 𝑁2 𝜕𝜓1 𝜕𝑦 = 0 𝜕2𝜃1 𝜕𝑦2 + 𝑁𝑡 𝜕𝜃0 𝜕𝑦 2 = 0 𝜓1 = − 𝐹1 2 , 𝜕𝜓1 𝜕𝑦 = 0, 𝜃1 = 0 𝑎𝑡 𝑦 = ℎ1 𝜓1 = 𝐹1 2 , 𝜕𝜓1 𝜕𝑦 = 0, 𝜃1 = 0 𝑎𝑡 𝑦 = ℎ2 With corresponding convective boundary conditions