working helmholtz

This commit is contained in:
max
2026-05-09 02:25:56 +02:00
parent 77ef4753a3
commit cf1bf30c81
3 changed files with 121 additions and 103 deletions

View File

@@ -6,6 +6,12 @@ namespace FluidSim.Core
{
public class BoundarySystem
{
// ---------- Private constants ----------
private const float Gamma = 1.4f;
private const float Gm1 = Gamma - 1f; // 0.4
private const float Rgas = 287f; // J/(kg·K)
private const float GammaOverGm1 = Gamma / Gm1; // 3.5
public struct OrificeDesc
{
public Port VolumePort;
@@ -19,8 +25,8 @@ namespace FluidSim.Core
public float EffectiveLength;
public float CurrentMdot; // kg/s, positive = volume → pipe
// --- Dissipative loss ---
public float LossCoefficient; // K factor for pressure drop = K * 0.5*rho*u^2
// --- Loss coefficient (linear resistance) ---
public float LossCoefficient; // N·s/m⁵ or kg/(m⁴·s)
}
public struct OpenEndDesc
@@ -50,6 +56,7 @@ namespace FluidSim.Core
public int OrificeCount { get; private set; }
public int OpenEndCount { get; private set; }
// ---------- Add orifice (no inertance) ----------
public void AddOrifice(Port volumePort, int pipeIndex, bool isLeftEnd,
int areaIndex, float dischargeCoeff = 1f,
float lossCoefficient = 0f)
@@ -69,14 +76,17 @@ namespace FluidSim.Core
OrificeCount++;
}
// ---------- Add orifice with inertance ----------
public void AddOrificeWithInertance(Port volumePort, int pipeIndex, bool isLeftEnd,
int areaIndex, float dischargeCoeff,
float effectiveLength, float lossCoefficient = 0f)
{
// Reuse the base AddOrifice and then override fields
AddOrifice(volumePort, pipeIndex, isLeftEnd, areaIndex, dischargeCoeff, lossCoefficient);
ref var d = ref _orifices[OrificeCount - 1];
d.UseInertance = true;
d.EffectiveLength = effectiveLength;
d.LossCoefficient = lossCoefficient; // store the linear resistance
}
public void AddOpenEnd(int pipeIndex, bool isLeftEnd,
@@ -112,15 +122,33 @@ namespace FluidSim.Core
return _openEnds[openEndIndex].LastFacePressure;
}
// ---------- Resolve all orifices ----------
public void ResolveOrifices(float dt)
{
for (int i = 0; i < OrificeCount; i++)
{
ref var d = ref _orifices[i];
float area = _orificeAreas[d.AreaIndex];
// Gather volume state
float volP = d.VolumePort?.Pressure ?? 101325f;
float volRho = d.VolumePort?.Density ?? 1.2f;
float volT = d.VolumePort?.Temperature ?? 300f;
float volH = d.VolumePort?.SpecificEnthalpy ?? 0f;
float volAF = d.VolumePort?.AirFraction ?? 1f;
// Gather pipe interior state
var (pipeRho, pipeU, pipeP) = d.IsLeftEnd
? _pipeSystem.GetInteriorStateLeft(d.PipeIndex)
: _pipeSystem.GetInteriorStateRight(d.PipeIndex);
float pipeT = pipeP / MathF.Max(pipeRho * Rgas, 1e-12f);
float pipeAF = d.IsLeftEnd
? _pipeSystem.GetInteriorAirFractionLeft(d.PipeIndex)
: _pipeSystem.GetInteriorAirFractionRight(d.PipeIndex);
// ---- Handle closed orifice (area ≈ 0) as a wall ----
if (area < 1e-12f || d.VolumePort == null)
{
// Closed wall reflect interior state
var (rInt, uInt, pInt) = d.IsLeftEnd
? _pipeSystem.GetInteriorStateLeft(d.PipeIndex)
: _pipeSystem.GetInteriorStateRight(d.PipeIndex);
@@ -137,143 +165,126 @@ namespace FluidSim.Core
continue;
}
// Gather states
float volP = d.VolumePort.Pressure;
float volRho = d.VolumePort.Density;
float volT = d.VolumePort.Temperature;
float volH = d.VolumePort.SpecificEnthalpy;
float volAF = d.VolumePort.AirFraction;
var (pipeRho, pipeU, pipeP) = d.IsLeftEnd
? _pipeSystem.GetInteriorStateLeft(d.PipeIndex)
: _pipeSystem.GetInteriorStateRight(d.PipeIndex);
float pipeT = pipeP / MathF.Max(pipeRho * 287f, 1e-12f);
float pipeAF = d.IsLeftEnd
? _pipeSystem.GetInteriorAirFractionLeft(d.PipeIndex)
: _pipeSystem.GetInteriorAirFractionRight(d.PipeIndex);
float gamma = 1.4f, R = 287f, Cd = d.DischargeCoeff;
// --- Preliminary nozzle solution (no loss) to estimate flow direction and velocity ---
// ---- Preliminary isentropic solution (used for face pressure if inertance is on) ----
float mdotEst, rhoFaceEst, uFaceEst, pFaceEst;
if (volP >= pipeP)
{
IsentropicOrifice.Compute(volP, volRho, volT, pipeP, gamma, R, area, Cd,
IsentropicOrifice.Compute(volP, volRho, volT, pipeP, Gamma, Rgas, area, d.DischargeCoeff,
out mdotEst, out rhoFaceEst, out uFaceEst, out pFaceEst);
}
else
{
IsentropicOrifice.Compute(pipeP, pipeRho, pipeT, volP, gamma, R, area, Cd,
IsentropicOrifice.Compute(pipeP, pipeRho, pipeT, volP, Gamma, Rgas, area, d.DischargeCoeff,
out mdotEst, out rhoFaceEst, out uFaceEst, out pFaceEst);
mdotEst = -mdotEst;
}
// --- Apply symmetric loss if LossCoefficient > 0 ---
float volP_eff = volP;
float pipeP_eff = pipeP;
if (d.LossCoefficient > 0f && MathF.Abs(mdotEst) > 1e-12f)
{
float rhoRef = mdotEst >= 0 ? rhoFaceEst : rhoFaceEst; // rhoFaceEst already reflects the correct side
float uRef = uFaceEst;
float dynP = 0.5f * rhoRef * uRef * uRef * d.LossCoefficient;
// ---- Compute ghost state ----
float mdotFinal, rhoFace, uFace, pFace, airFracGhost;
// Clamp the loss to avoid overshoot (max 80% of pressure difference)
float dp = MathF.Abs(volP - pipeP);
dynP = MathF.Min(dynP, 0.8f * dp);
// Apply symmetrically: loss reduces the higher pressure and increases the lower pressure
if (mdotEst >= 0) // volume → pipe
{
volP_eff -= dynP;
pipeP_eff += dynP;
}
else // pipe → volume
{
pipeP_eff -= dynP;
volP_eff += dynP;
}
}
// --- Final nozzle solution with corrected pressures ---
float mdotSS, rhoFace0, uFace0, pFace0;
if (volP_eff >= pipeP_eff)
{
IsentropicOrifice.Compute(volP_eff, volRho, volT, pipeP_eff, gamma, R, area, Cd,
out float mUp, out rhoFace0, out uFace0, out pFace0);
mdotSS = mUp;
}
else
{
IsentropicOrifice.Compute(pipeP_eff, pipeRho, pipeT, volP_eff, gamma, R, area, Cd,
out float mUp, out rhoFace0, out uFace0, out pFace0);
mdotSS = -mUp;
}
float mdot;
if (d.UseInertance)
{
// ---- Inertance ODE with loss ----
float rhoUp = d.CurrentMdot >= 0 ? volRho : pipeRho;
float inertance = rhoUp * d.EffectiveLength / area;
float dp = volP_eff - pipeP_eff;
float resistance = MathF.Abs(dp) / MathF.Max(MathF.Abs(mdotSS), 1e-12f);
float dmdot_dt = (dp - resistance * d.CurrentMdot) / inertance;
mdot = d.CurrentMdot + dmdot_dt * dt;
float inertance = rhoUp * d.EffectiveLength / MathF.Max(area, 1e-12f);
float dp = volP - pipeP;
float Rlin = d.LossCoefficient; // linear resistance
// Forward Euler
float dmdot_dt = (dp - Rlin * d.CurrentMdot) / MathF.Max(inertance, 1e-12f);
float mdotNew = d.CurrentMdot + dmdot_dt * dt;
// ---------- Symmetric flow limiter ----------
// 1) limit by cavity mass
if (d.VolumePort.Owner is Volume0D vol0)
{
float maxOut = vol0.Mass / dt;
if (mdot > maxOut) mdot = maxOut;
if (mdotNew > maxOut) mdotNew = maxOut; // cavity → pipe
if (mdotNew < -maxOut) mdotNew = -maxOut; // pipe → cavity
}
if (float.IsNaN(mdot)) mdot = 0f;
// 2) limit by mass in the adjacent pipe cell
int adjCell = d.IsLeftEnd ? _pipeSystem.GetPipeStart(d.PipeIndex)
: _pipeSystem.GetPipeEnd(d.PipeIndex) - 1;
float pipeRhoAdj = _pipeSystem.GetCellDensity(adjCell);
float pipeDxAdj = _pipeSystem.GetCellDx(adjCell); // uses the new public method
float pipeCellMass = pipeRhoAdj * area * pipeDxAdj;
float maxFromPipe = pipeCellMass / dt;
if (mdotNew < -maxFromPipe) mdotNew = -maxFromPipe; // prevent emptying the pipe cell
// NaN safety
if (float.IsNaN(mdotNew)) mdotNew = 0f;
// Store for next step
d.CurrentMdot = mdotNew;
mdotFinal = mdotNew;
// Ghost state: use the isentropic face pressure (pFaceEst) as reference,
// but compute velocity from mdotFinal.
rhoFace = mdotFinal >= 0 ? volRho : pipeRho;
pFace = pFaceEst; // approximate face pressure
uFace = MathF.Abs(mdotFinal) / MathF.Max(rhoFace * area, 1e-12f);
}
else
{
mdot = mdotSS;
// ---- Standard quasisteady orifice ----
mdotFinal = mdotEst;
rhoFace = rhoFaceEst;
uFace = uFaceEst;
pFace = pFaceEst;
// Limit outflow from cavity
if (d.VolumePort.Owner is Volume0D vol0)
{
float maxOut = vol0.Mass / dt;
if (mdot > maxOut) mdot = maxOut;
if (mdotFinal > maxOut) mdotFinal = maxOut;
}
d.CurrentMdot = mdotFinal;
}
d.CurrentMdot = mdot; // stored for future steps (inertance or loss)
// Ghost state construction
float rhoFace = mdot >= 0 ? volRho : pipeRho;
float pFace = pFace0;
float uFace = MathF.Abs(mdot) / MathF.Max(rhoFace * area, 1e-12f);
float airFracGhost;
if (mdot >= 0)
// ---- Determine air fraction for ghost ----
if (mdotFinal >= 0)
{
airFracGhost = volAF;
}
else
{
airFracGhost = pipeAF;
d.VolumePort.AirFraction = pipeAF;
if (d.VolumePort != null) d.VolumePort.AirFraction = pipeAF;
}
if (mdot >= 0 && d.IsLeftEnd) uFace = +uFace;
else if (mdot >= 0 && !d.IsLeftEnd) uFace = -uFace;
else if (mdot < 0 && d.IsLeftEnd) uFace = -uFace;
else if (mdot < 0 && !d.IsLeftEnd) uFace = +uFace;
// ---- Apply sign convention for velocity ----
if (mdotFinal >= 0 && d.IsLeftEnd) uFace = +uFace;
else if (mdotFinal >= 0 && !d.IsLeftEnd) uFace = -uFace;
else if (mdotFinal < 0 && d.IsLeftEnd) uFace = -uFace;
else if (mdotFinal < 0 && !d.IsLeftEnd) uFace = +uFace;
// ---- Set ghost cells ----
if (d.IsLeftEnd)
_pipeSystem.SetGhostLeft(d.PipeIndex, rhoFace, uFace, pFace, airFracGhost);
else
_pipeSystem.SetGhostRight(d.PipeIndex, rhoFace, uFace, pFace, airFracGhost);
d.VolumePort.MassFlowRate = -mdot;
if (-mdot >= 0)
// ---- Update volume port (mass flow: positive into volume) ----
if (d.VolumePort != null)
{
float pipeH = gamma / (gamma - 1f) * pipeP / MathF.Max(pipeRho, 1e-12f);
d.VolumePort.SpecificEnthalpy = pipeH;
}
else
{
d.VolumePort.SpecificEnthalpy = volH;
d.VolumePort.MassFlowRate = -mdotFinal;
// Set enthalpy of the stream entering the volume
if (-mdotFinal >= 0) // mass flowing into the volume (out of pipe)
{
float pipeH = GammaOverGm1 * pipeP / MathF.Max(pipeRho, 1e-12f);
d.VolumePort.SpecificEnthalpy = pipeH;
}
else // mass flowing out of the volume (into pipe)
{
d.VolumePort.SpecificEnthalpy = volH;
}
}
}
}
// ---------- Resolve open ends ----------
public void ResolveOpenEnds(float dt)
{
for (int i = 0; i < OpenEndCount; i++)
@@ -303,6 +314,7 @@ namespace FluidSim.Core
bool supersonic = d.IsLeftEnd ? (uInt <= -cInt) : (uInt >= cInt);
float rhoGhost, uGhost, pGhost, afGhost;
if (supersonic)
{
rhoGhost = rhoInt; uGhost = uInt; pGhost = pInt; afGhost = afInt;

View File

@@ -149,6 +149,7 @@ namespace FluidSim.Core
public int GetPipeEnd(int pipeIdx) => _pipeEnd[pipeIdx];
public float GetCellPressure(int i) => _p[i];
public float GetCellDensity(int i) => _rho[i];
public float GetCellDx(int i) => _dx[i];
public float GetCellVelocity(int i)
{
float rho = _rho[i];

View File

@@ -57,18 +57,23 @@ namespace FluidSim.Tests
float rho0 = 101325f / (287f * 300f);
pipeSystem = new PipeSystem(neckCells, pipeStart, pipeEnd, areas, dxs, rho0, 0f, 101325f);
// Energy loss
cavity.EnergyRelaxationRate = 80f;
pipeSystem.EnergyRelaxationRate = 0f;
pipeSystem.DampingMultiplier = 2000f;
// --- Boundary system ---
boundaries = new BoundarySystem(pipeSystem, maxOrifices: 1, maxOpenEnds: 1);
float ComputeResistance(float decayTimeSeconds, float rho, float L_eff, float A)
{
// R = 2 * rho * L_eff / (A * decayTimeSeconds)
return 2f * rho * L_eff / (A * MathF.Max(decayTimeSeconds, 1e-6f));
}
// Use steady orifice the pipe already provides the inertia
boundaries.AddOrifice(cavityPort, pipeIndex: 0, isLeftEnd: true, areaIndex: cavityOrificeIdx, dischargeCoeff: 1f, lossCoefficient: 0.1f);
// LOSS COEFFICIENT BREAKS THE SYSTEM AT ~0.55, AT VALUES LOWER THAN THAT, IT SEEMS TO ONLY AFFECT VOLUME, NOT COMPOUND
boundaries.AddOrificeWithInertance(
cavityPort, pipeIndex: 0, isLeftEnd: true,
areaIndex: cavityOrificeIdx,
dischargeCoeff: 0.9f,
effectiveLength: neckLength, // physical length (or L_eff)
lossCoefficient: 9000 // start with this, adjust for decay time
);
// Open end at right side of pipe
boundaries.AddOpenEnd(pipeIndex: 0, isLeftEnd: false, 101325f, neckArea);
@@ -78,7 +83,7 @@ namespace FluidSim.Tests
// --- Solver ---
// Slightly higher substep count to ensure stability of the resonant oscillation
solver = new Solver { SubStepCount = 6, EnableProfiling = true };
solver = new Solver { SubStepCount = 6, EnableProfiling = false };
solver.SetTimeStep(dt);
solver.SetPipeSystem(pipeSystem);
solver.SetBoundarySystem(boundaries);