Fundamental Principles & Equations < Aerodynamic Tools...
Transcript of Fundamental Principles & Equations < Aerodynamic Tools...
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Aerodynamics 2015 fall - 1 -
Fundamental Principles & Equations
< Aerodynamic Tools >
BasicEquation
UsefulConcept
ComputationalFluid Dynamics
ExperimentalTechniques
Continuity Eqn.
Momentum Eqn.
Energy Eqn.
StreamlinesVorticity
CirculationStream fn.
Velocity Potential
FDMFVMBEMFEMPanel
FlowVisualization
Force & MomentMeasurement
PressureDensity Measurementvelocity
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Aerodynamics 2015 fall - 2 -
Fundamental Principles & Equations
< 2.1. Vector Relations >
Orthogonal Coordinate
* Cartesian coordinate * Cylindrical coordinate * Spherical coordinate
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Aerodynamics 2015 fall - 3 -
Fundamental Principles & Equations
< 2.2. Scalar & Vector Fields >
* Scalar quantities
* Vector quantities
* Products
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Aerodynamics 2015 fall - 4 -
< 2.2. Scalar & Vector Fields >
Fundamental Principles & Equations
* Gradient
* Curl : rate of change of fluid element
* Divergence : rate of volume change
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Aerodynamics 2015 fall - 5 -
< 2.2. Scalar & Vector Fields >
Fundamental Principles & Equations
* Line integral
* Surface integral
* Volume integral
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Aerodynamics 2015 fall - 6 -
Fundamental Principles & Equations
< 2.2. Scalar & Vector Fields >
* Relation between line, surface, and volume integral
* Stokes Theorem
* Divergence Theorem
* Gradient Theorem
* Control Volume vs Material Volume (or Control Mass)
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Aerodynamics 2015 fall - 7 -
Fundamental Principles & Equations
< 2.3. Models of the fluid >
• Conservation of mass
• Conservation of momentum
• Conservation of energy
RealPhysics
Fluid Model
FundamentalEquation
or Princiles
Mass
Momentum
Energy
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Aerodynamics 2015 fall - 8 -
Fundamental Principles & Equations
< 2.3. Models of the fluid >
Fluid Model
Finite Control Volume – fixed with space (Eulerian
Description)
Finite Material Volume – moving with fluid (Lagrangian
Description)
Infinitesimal Fluid Element
Molecular approach – statistical view, Boltzmann
Equation
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Aerodynamics 2015 fall - 9 -
< 2.3. Models of the fluid >
Physical Meaning of Divergence of Velocity
The total change of the whole control
volume over time ∆t
Think an infinitesimal volume
is the time rate of change of the volume of a moving fluid element
Fundamental Principles & Equations
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Aerodynamics 2015 fall - 10 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
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Aerodynamics 2015 fall - 11 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Mass flow
The plane of fluid particles which are on the surface at time
t will move off the surface at time t+Δt, sweeping out a
volume given by Δv=VnAΔt.
( where Vn=V·n )
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Aerodynamics 2015 fall - 12 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Mass flow
The mass of fluid in this swept volume, which evidently
passed through the area during the Δt interval, is
tAVvm n
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Aerodynamics 2015 fall - 13 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Mass flow
The mass flow is defined as the time rate of this mass
passing though the area.
The mass flux is defined simply as mass flow per area.
AVt
mmflowmass n
t
0lim
nVA
mfluxmass
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Aerodynamics 2015 fall - 14 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Principle #1 : Mass should be conserved
Consider a control volume,
Net increase in the contorl volume = In - Out
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Aerodynamics 2015 fall - 15 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Principle #1 : Mass should be conserved
Increase of mass in CV
Net flow = outflow - inflow
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Aerodynamics 2015 fall - 16 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Principle #1 : Mass should be conserved
* fixed volume
* divergence theorem
To satisfy with arbitrary control volume
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Aerodynamics 2015 fall - 17 -
Fundamental Principles & Equations
< 2.4. Continuity equation >
Principle #1 : Mass should be conserved
0
0
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Aerodynamics 2015 fall - 18 -
Fundamental Principles & Equations
< 2.5. Momentum equations >
Principle #2 :
Time rate of momentum change = Force
Rate of momentum change inside the control volume
Net flow of momentum = ( )in – ( )out
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Aerodynamics 2015 fall - 19 -
Fundamental Principles & Equations
< 2.5. Momentum equations >
Force acting on the control volume
• Body force : acting on the body
gravity, electromagnetic force
• Surface force : shear stress (due to viscosity)
Opposite direction to the surface
* Integral Form of Momentum Equation
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Aerodynamics 2015 fall - 20 -
Fundamental Principles & Equations
< 2.5. Momentum equations >
Gradient Theorem
Divergence Theorem
* Differential Form of Momentum Equation
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Aerodynamics 2015 fall - 21 -
Fundamental Principles & Equations
< 2.5. Momentum equations >
• Divergence of a dyadic becomes a vector using the relation of
* dyadic (momentum flux tensor)
* u-direction :
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Aerodynamics 2015 fall - 22 -
Fundamental Principles & Equations
< 2.7. Energy equation >
Principle : Energy is conserved
Gibb’s Equation
Rate of heatadded to fluidinside CVfrom surrounding
Rate of work doneon fluid insidecontrol volue
Rate of change ofEnergy of fluid as it flows through CV
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Aerodynamics 2015 fall - 23 -
Fundamental Principles & Equations
< 2.7. Energy equation >
Rate of volumetric heating
Pressure term
Viscous heat addition
Body force term Viscous work term
Time rate of changeof total energyinside CV
Net rate of changeof total energyacross CV
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Aerodynamics 2015 fall - 24 -
Fundamental Principles & Equations
< 2.7. Energy equation >
* Integral Form of energy equation
* Differential Form of energy equation
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Aerodynamics 2015 fall - 25 -
Fundamental Principles & Equations
< 2.7. Energy equation >
* Differential Form of energy equation
If steady,
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Aerodynamics 2015 fall - 26 -
Fundamental Principles & Equations
Now 6 unknowns 5 equations +1
Continuity equation
Momentum equation
Energy equation
Equation of state