analyticalSol Class Reference

Class analytical solutions for the Physalis cage points. More...

#include <analyticalSol.h>

List of all members.

Public Member Functions

 analyticalSol ()
void solve (vector< real > &p, const vector< real > &rP, const vector< real > &thetaP, const vector< real > &phiP, vector< real > &omegaX, const vector< real > &rOmegaX, const vector< real > &thetaOmegaX, const vector< real > &phiOmegaX, vector< real > &omegaY, const vector< real > &rOmegaY, const vector< real > &thetaOmegaY, const vector< real > &phiOmegaY, vector< real > &omegaZ, const vector< real > &rOmegaZ, const vector< real > &thetaOmegaZ, const vector< real > &phiOmegaZ, vector< real > &u, const vector< real > &rU, const vector< real > &thetaU, const vector< real > &phiU, vector< real > &v, const vector< real > &rV, const vector< real > &thetaV, const vector< real > &phiV, vector< real > &w, const vector< real > &rW, const vector< real > &thetaW, const vector< real > &phiW, int nTruncate, real ReynoldsNumber, vector< real > &solvedABCoeffOneParticle, vector< real > &UFixedParticles, vector< real > &SFixedParticles, vector< real > &VFixedParticles, int &fixedParticles, int rotatingParticles, int particle, real **angVel, real **angVelAcc, real **torqueOld, real **torqueNew)
 ~analyticalSol ()


Detailed Description

Class analytical solutions for the Physalis cage points.

This class receives the finite-difference solutions of pressure and vorticity, solves the analytical solutions of velocity in the cage points, and returns these analytical solutions as the boundary conditions of the finite-difference scheme of the flow field.


Constructor & Destructor Documentation

analyticalSol::analyticalSol (  ) 

constructor

analyticalSol::~analyticalSol (  ) 

destructor


Member Function Documentation

void analyticalSol::solve ( vector< real > &  p,
const vector< real > &  rP,
const vector< real > &  thetaP,
const vector< real > &  phiP,
vector< real > &  omegaX,
const vector< real > &  rOmegaX,
const vector< real > &  thetaOmegaX,
const vector< real > &  phiOmegaX,
vector< real > &  omegaY,
const vector< real > &  rOmegaY,
const vector< real > &  thetaOmegaY,
const vector< real > &  phiOmegaY,
vector< real > &  omegaZ,
const vector< real > &  rOmegaZ,
const vector< real > &  thetaOmegaZ,
const vector< real > &  phiOmegaZ,
vector< real > &  u,
const vector< real > &  rU,
const vector< real > &  thetaU,
const vector< real > &  phiU,
vector< real > &  v,
const vector< real > &  rV,
const vector< real > &  thetaV,
const vector< real > &  phiV,
vector< real > &  w,
const vector< real > &  rW,
const vector< real > &  thetaW,
const vector< real > &  phiW,
int  nTruncate,
real  ReynoldsNumber,
vector< real > &  solvedABCoeffOneParticle,
vector< real > &  UFixedParticles,
vector< real > &  SFixedParticles,
vector< real > &  VFixedParticles,
int &  fixedParticles,
int  rotatingParticles,
int  particle,
real **  angVel,
real **  angVelAcc,
real **  torqueOld,
real **  torqueNew 
)

Receives finite-difference solutions, obtains the analytical velocity for the Stokes equation, and returns these analytical solution to the finite-difference scheme

construct analytical solution in one cage for pressure, vorticity, velocities at those cage points

write everything in the form, using pressure as an example, p = pWeight dotproduct ABCoeff where pWeight = [pWeightA0, pWeightB0, pWeightA1, pWeightATilde1,pWeightB1, pWeightBTilde1, pWeightAK, pWeightATildeK,pWeightBK, pWeightBTildeK] and ABCoeff = [A0, B0, A1, ATilde1,B1, BTilde1, AK, ATildeK,BK, BTildeK] where B0 denotes p0 * Re^2

similarly, vorticity = omegaWeight dotproduct ABCoeff, uR = uRWeight dotproduct ABCoeff , uTheta = uThetaWeight dotproduct ABCoeff, u = uWeight dotproduct ABCoeff, v = vWeight dotproduct ABCoeff,

ABCoeff is to be determined from weightMatrix ABCoeff = b

note that r is the normalized distance from the origin

Formula are in spherical coordinate: p, u, v, w, omegaX, omegaY, and omegaZ.

all input and output fields of pressure, velocity, and vorticity are from the finite-difference scheme i.e., in the original inertial frame

Parameters:
p  pressure
rP  r value of pressure points
thetaP  theta value of pressure points
phiP  phi value of pressure points
omegaX  omegaX
rOmegaX  r value of omegaX points
thetaOmegaX  theta value of omegaX points
phiOmegaX  phi value of omegaX points
omegaY  omegaY
rOmegaY  r value of omegaY points
thetaOmegaY  theta value of omegaY points
phiOmegaY  phi value of omegaY points
omegaZ  omegaZ
rOmegaZ  r value of omegaZ points
thetaOmegaZ  theta value of omegaZ points
phiOmegaZ  phi value of omegaZ points
u  u
rU  r value of u points
thetaU  theta value of u points
phiU  phi value of u points
v  v
rV  r value of v points
thetaV  theta value of v points
phiV  phi value of v points
w  w
rW  r value of w points
thetaW  theta value of w points
phiW  phi value of w points
nTruncate  Order of the truncated spertral solutions
ReynoldsNumber  Reynolds number
solvedABCoeffOneParticle  Coefficiences of A, B, and C
UFixedParticles  stores U of the LLS solver
SFixedParticles  stores S of the LLS solver
VFixedParticles  stores V of the LLS solver
fixedParticles  stores if the particles are fixed
rotatingParticles  stores if the particles are rotating
particle  m-th particles
angVel  angular velocity of particles
angVelAcc  angular velocity acceleration of particles
torqueOld  torque value in previous iteration of particles
torqueNew  torque value in current iteration of particles


The documentation for this class was generated from the following files:

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