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2.29 Numerical Fluid Fall 2011 – Lecture 6 REVIEW of Lecture 5 • Continuum Hypothesis and conservation laws • Macroscopic Properties Material covered in class: Differential forms of conservation laws • Material (substantial/) • – Differential Approach – Integral () Approach • Use of Gauss Theorem – Incompressibility • Reynolds Transport Theorem • Conservation of (Cauchy’s Momentum equations) • The Navier-Stokes equations – Constitutive equations: – Navier-stokes, compressible and incompressible

2.29 Numerical PFJL Lecture 6, 1

1 Fluid flow modeling: the Navier-Stokes equations and their approximations – Cont’d Today’s Lecture

• References : – Chapter 1 of “J. H. Ferziger and M. Peric, Computational Methods for . Springer, New York, third edition, 2002.” – Chapter 4 of “I. M. Cohen and P. K. Kundu. Fluid Mechanics. Academic Press, Fourth Edition, 2008” – Chapter 4 in “F. M. White, Fluid Mechanics. McGraw-Hill Companies Inc., Sixth Edition” • For today’s lecture, any of the chapters above suffice – Note each provide a somewhat different perspective

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 2

2 Integral Conservation Law for a scalar 

 d  d    dV   dV   (.v n )dA   q  .n dA  s dV  CM  CV CS CS CV dt  dt fixed  fixed Advective fluxes Other transports (, etc)  ("convective" fluxes) Sum of sources and sinks terms (reactions, etc)

Applying the Gauss Theorem, for any arbitrary CV gives: ρ,Φ v    .(v)  . q  s CV,   s t fixed Φ  q For a common diffusive flux model (Fick’s law, Fourier’s law):  q  k 

 Conservative form  .(v) .(k )  s of the PDE t 

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 3

3 Strong-Conservative form of the Navier-Stokes Equations (  v) d  Cons. of Momentum: vdV   v (.)v n dA   p ndA  .ndA  gdV dt CV CS CS CS CV   F   Applying the Gauss Theorem gives:  p  . g dV CV

v  For any arbitrary CV gives: .(  vv ) p .  g t ρ,Φ v With Newtonian fluid + incompressible + constant μ: CV,  sΦ v  2   fixed  Momentum: .(vv)  p   v  g q t Mass: .v 0

Equations are said to be in “strong conservative form” if all terms have the form of the divergence of a vector or a . For the i th Cartesian component, in the general Newtonian fluid case:

 v   u u  2 u  With Newtonian fluid only: i .(  vv )   .  p e    i  j e   j e   gx e  t i  i  x x  j 3 x i i i i    j i  j  2.29 Numerical Fluid Mechanics PFJL Lecture 6, 4

4 Navier-Stokes Equations: For an Incompressible Fluid with constant

V(x,y,z) Fluid Velocity Field

Hydrostatic : -g z for z positive upward Conservation of Mass

Dynamic Pressure P = Pactual -gz

Navier-Stokes Equation

Kinematic viscosity  Density 

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 5

5 Incompressible Fluid Pressure Equation

Navier-Stokes Equation

Conservation of Mass

Divergence of Navier-Stokes Equation

V)V== - Dynamic Pressure Poisson Equation

More general than Bernoulli – Valid for unsteady and rotational flow

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 6

6 Incompressive Fluid Equation

Vorticity

Navier-Stokes Equation

curl of Navier-Stokes Equation

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 7

7 Inviscid Fluid Mechanics Euler’s Equation

Navier-Stokes Equation: incompressible, constant viscosity

If also inviscid fluid

 Euler’s Equations

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 8

8 Inviscid Fluid Mechanics Bernoulli Theorems

Theorem 1 Theorem 2

Irrotational Flow, incompressible Steady, Incompressible, inviscid, no shaft work, no

Flow Potential Navier-Stokes Equation

Define X

Along stream lines and vortex lines

Introduce PT = Thermodynamic pressure

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 9

9 Potential Flows Integral Equations

Irrotational Flow

Flow Potential

Conservation of Mass “Mostly” Potential Flows: Only rotation occurs at boundaries due to viscous terms

In 2D:   Velocity potential : u  , v  x y Laplace Equation   Stream function : u  , v  y x

• Since Laplace equation is linear, it can be solved by superposition of flows, called panel methods • What distinguishes one flow from another are the boundary conditions and the geometry: there are no intrinsic parameters in the Laplace equation

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 10

10 Potential Flow Boundary Integral Equations

Green’s Theorem

n

Green’s Function

Homogeneous Solution

S

V Boundary Integral Equation

Discretized Integral Equation

Linear System of Equations

Panel Methods

2.29 Numerical Fluid Mechanics PFJL Lecture 6, 11

11 MIT OpenCourseWare http://ocw.mit.edu

2.29 Numerical Fluid Mechanics Fall 2011

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