potential analogies
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Incomplete Word notes by Phil dated 8.5.10, meant to be read in split-screen to compare physical settings of the potential equation. It lines up electrostatics, heat flow and fluid flow: potential, current and flux, conductivity, sources, and Dirichlet versus Neumann boundary conditions. It also covers insulated and charge-free boundaries and cites Stakgold vol. I p. 328.
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Potential Problem Analogies PhL 8.5.10
This is very incomplete. Use split-screen to compare two worlds.
1. Electrostatics:
potential V
potential difference ΔV drives electric current dQ/dt via ohms law
current I = dQ/dt = ΔV /R
surface of metal is place where V = constant
electric field E = -V = electric flux density, constant = 1
current density J = κE constant = κ = electric conductivity
∂nV = En = 4πσ at a metal boundary surface, σ = charge density = electric flux source
2V ~ ρ = 3D charge density
∂nV ~ σ = charge density source
Dirichlet BC: specify V on boundary
Neumann BC: charge density flow on boundary
positive and negative charge
charge-free boundary (such as cap of bowl) has ∂nV = 0
2. Heat flow:
temperature u
temperature difference Δu drives heat current dQ/dt via the conduction heat transfer law
heat current I = dQ/dt = Δu/R R = thermal resistor resistance
surface against heat reservoir is place where u = constant
heat flow field F = - k u(x) constant = k = thermal conductivity
heat current density J = F constant = 1
∂nu = heat current source at a boundary = (-1/k) Fn = like charge density σ but has no name
( heat flow: ∂tQ = -k ∂nu ∂tQ is like σ, heat flow through unit area of surface. )
2u = 3D heat source density = q(x)
∂tu - (k/c)2u = f(x,t)/c = 3D heat source // Stak v I p 328
static temperature distribution: - (k/c)2u = f(x,t)/c f ~ ρ
-k2u = f(x,t)
dimensions: f = energy/vol/time. k = energy/time/degree TBC
Dirichlet BC: specify u on boundary
Neumann BC: specify heat flow ∂nu on boundary
positive and negative heat flow source (source and sink)
insulated boundary means ∂nu = 0 since no heat flow cross boundary. (Neumann)
3. Fluid flow
velocity field v is like E
v = φ φ is the velocity potential
hard boundary wall sets vperp = 0 = ∂nφ = Neumann with σ = 0
∂nφ ~ source at a boundary
also at wall we have vparallel = 0 like we have Eparallel= 0 at a metal wall.
(so this is true where the wall has no source or sink, ie, it is not a leaky wall)