Windtunnel/Boundary Conditions: Difference between revisions
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(HG_3D) |
m (→empty circular tube: dp/L) |
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$$ | $$ | ||
v(r) = \frac{\ | v(r) = \frac{\Delta p}{L}\frac{R^2-r^2}{4\mu} | ||
$$ | $$ | ||
with \(\mu\)=dynamical viscosity | with \(\mu\)=dynamical viscosity |
Revision as of 09:53, 2 October 2024
New Keywords
in pluto.ini
ObjectType_int
: 0=nothing, 1=cylinder/sphere, 2=square/cube of sizeObjectDiameter_cm
WindPressure_Pa
,WindPressure_mbar
(mutually exclusive): pressure at entry (left)PressureGradient_mbar_per_cm
positive (even though pressure drops from left to right)- Wind velocity is ramped up to
WindVelocity_m_per_s
over timeInjectionTime_s
WindTemperature_C
KinematicViscosity_m2_per_s
,DynamicViscosity_Pa_s
,Wall_BoundaryCondition
for tangential walls, value from {0,1,2,3}
(ignored if given values <0)
in init.c
- macro
SOLID
to enable an object - array
solid
containing value 1 or 0 for object matter being present/absent
Walls
tangential
Boundary condition for the wall | ||
---|---|---|
vx1 | vx2 | |
no-shear | zero-gradient | reflective |
no-slip | reflective | reflective |
no-wall | zero-gradient | zero-gradient |
one-way wall | zero-gradient | zero-gradient & no-inflow |
entry/exit
prescribed velocity at entry (left)
prescribe pressure drop (left to right)
- current simulation result: \(v_x\)-profile slightly asymmetric and \(v_x<0\) at one wall
Object
Open Questions
Reflective cells
Setting the vector \(\vec v_g\) in a ghost cell as \(\vec v_g=-\vec v\), with \(\vec v\) being the value in the adjacent real cell, yields \(\vec 0\) as interpolation right at the boundary. This works for plane walls. What to do in cases where a ghost cell has more than one real cell as nearest neighbor? This calls for discussion!
Analytical Solutions
empty 2D channel
empty circular tube
$$ v(r) = \frac{\Delta p}{L}\frac{R^2-r^2}{4\mu} $$
with \(\mu\)=dynamical viscosity