Fluid Simulation for Video Games (Part 8)

By Dr. Michael J. Gourlay

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Baroclinicity: Fluid Buoyancy

Heavier fluid sinks, and lighter fluid rises.

This article, the eighth in a series, explains how a vortex-based fluid simulation handles variable density in a fluid. Part 1 summarized fluid dynamics; Part 2 surveyed fluid simulation techniques, and Part 3 and Part 4 presented a vortex-particle fluid simulation with two-way fluid-body interactions that runs in real time. Part 5 profiled and optimized that simulation code. Part 6 described a differential method for computing velocity from vorticity, and Part 7 showed how to integrate a fluid simulation into a typical particle system.

This article introduces features to the simulations presented in previous articles: The fluid flow includes motion because of buoyancy-heavier fluid sinks, and lighter fluid rises. These new features facilitate visual effects with effects of variable density or (with additional rendering work) multiple fluids, such liquid-gas mixtures like water and air. It also lays the groundwork for upcoming features like thermal convection (hot air rises) and combustion (generating heat from chemical processes).

Using Vortices to Push Heavy Fluid Below Light Fluid

Remember that the simulation presented in these articles focuses on vorticity. How does the vorticity equation express this effect of pushing heavy fluid underneath light fluid?

Remember from Part 1 that by taking the curl of the momentum equation, you derive the vorticity equation:

The buoyancy term expresses the tendency, depicted in Figure 1, to create regions of overturning, where fluids with density out of equilibrium (that is, heavy fluid above light fluid) form rolling currents that tend toward bringing the fluid into equilibrium (that is, vortices push heavy fluid below light fluid).

Figure 1.Making fluid right-side up. Where the pressure gradient and density gradient are not parallel, vorticity forms to bring fluid into equilibrium. Fluid will try to rotate to push down the bulge.

Boussinesq Approximation
Notice that the buoyancy term includes a density gradient () and a pressure gradient (). The Boussinesq approximation assumes (among other things) that the fluid is in hydrostatic equilibrium-that is, that the pressure gradient force balances compression because of gravity, so :

This equation obviates the need to compute pressure or its gradients.

Note: The Boussinesq approximation assumes that density variations are small (compared to the ambient density). Furthermore, liquids, which are far more incompressible than gasses, have different density variations, but this simulation does not make that distinction. So, these simulations might violate these assumptions, in which case the simulation results depart even farther from scientific rigor. For visual effects in video games, though, where performance is king, we care about plausibility and aesthetics; so once again, we take drastic liberties and favor speed over accuracy.

Adding Fluid Buoyancy to the Simulation

To add the effects of fluid buoyancy, the simulation needs to track fluid density so that it can compute its gradient. From the previous version of the simulation, particles already have density, which is used to interact with solid bodies (as described in Part 4). The simulation reuses that density to populate a grid, and then computes density on that grid in much the same way vorticity is transferred to a grid to compute its spatial derivatives.

Representing Density Using Particles
As described in earlier articles, vorticity advects as a material property; vortex particles move in the same way mass does. So, the density associated with vortex particles suffices to provide all the density information you need.

For efficiency, use as few vortons as possible-just enough to make the simulation "look good." The grid will have cells that contain no vortons. But the fluid has mass everywhere, not just at or near vortons. So, you could write the simulation so that it ensures it has at least one vorton per cell, spontaneously creating vortons in any empty cells. But that would be expensive.

Instead, you can represent density in two parts: ambient and deviation. The ambient density acts like a default value for density in the absence of vortons. Vortons, meanwhile, represent density deviation from that ambient. The actual density is then ambient plus deviation. Consider, for example, a fluid with some uniform ambient density (as the gray area in Figure 2). Then introduce vortons that have a positive density deviation (as the blue vorton in Figure 2). Near those heavier vortons, the density of the fluid is above ambient. Now introduce vortons that have a negative density deviation (as the pink vorton in Figure 2). Near those lighter vortons, the density of the fluid is below ambient.

Figure 2.Density as ambient plus deviation. Fluid (the gray field) has an ambient density uniformly throughout. Vortons carry a value used as the deviation applied to that ambient value. The reddish vorton has a negative density deviation; therefore, fluid in that region is lighter than ambient. The bluish vorton has a positive density deviation; therefore, fluid in that region is heavier than ambient.

The code accompanying this article has a utility routine-Particle::GetMass-for computing the actual mass of a fluid particle, given the ambient density of the fluid, assuming that the particle density actually represents density deviation. The fluid-body collision routines from Part 4, which assumed that particle mass is their entire mass, have been changed for the present article to use the new approach of ambient plus deviation.

float Particle::GetMass( float ambientDensity ) const
    const float fMass = ( mDensity + ambientDensity ) * GetVolume() ;
    return fMass ;

Assigning Density to a Grid
As with vorticity, representing density to a grid simplifies computing spatial derivatives. So, you assign density to a UniformGrid. Some fluid techniques represent mass directly on a grid, not using particles. But, as Part 4 describes, that approach leads to artificially large numerical diffusion of mass-mass gets "blurry" and loses detail. In contrast, this simulation tracks mass with particles, avoiding that numerical diffusion; this particle-based simulation therefore retains more detail than grid-based simulations.

Remember from Part 6 that when assigning vorticity to a grid, the total circulation that vortons carry needs to match total circulation in the grid. Likewise, the total mass that the vortons carry needs to match total mass in the grid. When assigning mass from vorton to grid, you therefore multiply by the ratio of volumes of the vorton and grid cell, as shown in Figure 3.

Figure 3. Assigning mass from vortons to grid

The contribution of mass to each grid point depends on the proximity of the vorton to that grid point; grid points closer to a vorton get more mass from it. (As in Part 6, any grid cell can contain any number of vortices: 0, 1 or more. Also, as before, the grid automatically sizes itself each update to fit all particles.) In the code, UniformGrid::Accumulate applies that formula.

In the code, VortonSim::PopulateDensityGrid assigns density from vortons to a grid:

void VortonSim::PopulateDensityGrid( UniformGrid<  float    > & densityGrid
                                   , const Vector< Particle > & particles  )
    densityGrid.Clear() ; 
    densityGrid.CopyShape( mGridTemplate ) ;
    densityGrid.Init( 0.0f )               ;
    // The grid resulting from this operation must preserve the
    // same total mass that the particles represent, so multiply
    // by the ratio of the particle volume to gridcell volume.
    const float oneOverCellVolume   = 1.0f / densityGrid.GetCellVolume() ;
    // Populate density grid.
    const size_t numParticles = particles.Size() ;
    for( size_t uParticle = 0 ; uParticle < numParticles ; ++ uParticle )
    {   // For each particle in the array...
        const Particle  &   rParticle   = particles[ uParticle ] ;
        const Vec3      &   rPosition   = rParticle.mPosition   ;
        const unsigned      uOffset     = densityGrid.OffsetOfPosition( rPosition ) ;
        // Note that the formula below uses Particle::GetMass
        // instead of Particle::GetMass( ambientDensity ).
        // This is because we first want to accumulate the
        // deviation from ambient only.  The uniform ambient density
        // is irrelevant to the gradient anyway.  Also, this loop
        // only accumulates a quantity where particles exist,
        // but in the absence of particles, the fluid has mass anyway.
        const float volumeCorrectedDensity = rParticle.GetMass() * oneOverCellVolume ;
        densityGrid.Accumulate( rPosition , volumeCorrectedDensity ) ;
        // Likewise here we only want to accumulate the mass /deviations/ of particles,
        // since this will be compared later to the mass /deviations/ on the grid.

Computing Density Gradients
Computing baroclinic generation requires knowing density gradients, , at the location of each vorton. Because it is uniform, the ambient density does not contribute to the gradient, so omit it when assigning density to the grid.

The UniformGrid::ComputeGradient function wraps the worker routine, ComputeGradientInteriorSlice, which computes the gradient for a portion of the interior of the domain. Boundaries require special logic, and they're relatively small compared to the interior, so you needn't bother parallelizing them.

void ComputeGradient(        UniformGrid< Vec3  > & gradient
                     , const UniformGrid< float > & scalarVals )
    const size_t    dims[3] = { scalarVals.GetNumPoints( 0 )
                              , scalarVals.GetNumPoints( 1 )
                              , scalarVals.GetNumPoints( 2 )   } ;
    const size_t    dimsMinus1[3] = { scalarVals.GetNumPoints( 0 )-1
                                    , scalarVals.GetNumPoints( 1 )-1
                                    , scalarVals.GetNumPoints( 2 )-1 } ;

    // Compute derivatives for interior (i.e. away from boundaries).
    #if USE_TBB
        {   // Use Threading Building Blocks to parallelize the computation.
            const size_t numZ = dimsMinus1[2] - 1 ;
            // Estimate grain size.
            const size_t grainSize =  MAX2( 1 , numZ / gNumberOfProcessors ) ;
                tbb::blocked_range<size_t>( 1 , dimsMinus1[2] , grainSize )
        , UniformGrid_ComputeGradientInterior_TBB( gradient , scalarVals ) ) ;

    // Compute derivatives for boundaries: 6 faces of box.

The actual computation occurs inside ComputeGradientInteriorSlice. The "slice" approach facilitates parallelizing using Intel® Threading Building Blocks (Intel® TBB).

static void ComputeGradientInteriorSlice(       UniformGrid< Vec3  > & gradient
                                        , const UniformGrid< float > & val
                                        , size_t izStart , size_t izEnd )
    const Vec3      spacing                 = val.GetCellSpacing() ;
    // Avoid divide-by-zero when z size is effectively 0 (for 2D domains)
    const Vec3      reciprocalSpacing( 1.0f / spacing.x , 1.0f / spacing.y
                       , spacing.z > FLT_EPSILON ? 1.0f / spacing.z : 0.0f ) ;
    const Vec3      halfReciprocalSpacing( 0.5f * reciprocalSpacing ) ;
    const size_t    dims[3] = { val.GetNumPoints( 0 ) , val.GetNumPoints( 1 )
                              , val.GetNumPoints( 2 )   } ;
    const size_t    dimsMinus1[3] = { val.GetNumPoints( 0 )-1
                       , val.GetNumPoints( 1 )-1 , val.GetNumPoints( 2 )-1 } ;
    const size_t    numXY                   = dims[0] * dims[1] ;
    size_t          index[3] ;

    // Compute derivatives for interior (i.e. away from boundaries).
    for( index[2] = izStart ; index[2] < izEnd ; ++ index[2] )
        for( index[1] = 1 ; index[1] < dimsMinus1[1] ; ++ index[1] )
            ASSIGN_YZ_OFFSETS ;
            for( index[0] = 1 ; index[0] < dimsMinus1[0] ; ++ index[0] )
                ASSIGN_XYZ_OFFSETS ;

                Vec3 & rVector = gradient[ offsetX0Y0Z0 ] ;
                /* Compute d/dx */
                rVector.x = ( val[ offsetXPY0Z0 ] - val[ offsetXMY0Z0 ] )
                            * halfReciprocalSpacing.x ;
                /* Compute d/dy */
                rVector.y = ( val[ offsetX0YPZ0 ] - val[ offsetX0YMZ0 ] )
                            * halfReciprocalSpacing.y ;
                /* Compute d/dz */
                rVector.z = ( val[ offsetX0Y0ZP ] - val[ offsetX0Y0ZM ] )
                            * halfReciprocalSpacing.z ;

Compute the Baroclinic Generation of Vorticity
You again use Intel® TBB to parallelize computing the baroclinic term:

void VortonSim::GenerateBaroclinicVorticity( const float    & timeStep
                                           , const unsigned & uFrame  )
    if( fabsf( mGravAccel * mVelGrid.GetExtent() ) < FLT_EPSILON )
    {   // Domain is 2D and has no significant component along the gravity direction,
        // so baroclinic generation cannot occur in this Boussinesq approximation.
        return ;

    // Populate density grid.
    PopulateDensityGrid( mDensityGrid
                       , reinterpret_cast< Vector< Particle > & >( mVortons ) ) ;

    // Compute density gradient.
    mDensityGradientGrid.Clear() ; // Clear any stale velocity information
    mDensityGradientGrid.CopyShape( mGridTemplate ) ;
    mDensityGradientGrid.Init() ; // Reserve memory for density gradient grid.
    ComputeGradient( mDensityGradientGrid , mDensityGrid ) ;

    const size_t    numVortons      = mVortons.Size() ;

    #if USE_TBB
        // Estimate grain size based on size of problem and number of processors.
        const size_t grainSize =  MAX2( 1 , numVortons / gNumberOfProcessors ) ;
        // Fill vertex buffer using threading building blocks
        parallel_for( tbb::blocked_range<size_t>( 0 , numVortons , grainSize )
                     , VortonSim_GenerateBaroclinicVorticity_TBB( timeStep , this ) ) ;
        GenerateBaroclinicVorticitySlice( timeStep , 0 , numVortons ) ;

The VortonSim::GenerateBaroclinicVorticitySlice routine computes the baroclinic term of the vorticity equation applied to each vorton. This step transfers back from grid to particles, completing the cycle:

void VortonSim::GenerateBaroclinicVorticitySlice( float timeStep
                                                , size_t iPclStart , size_t iPclEnd )
    for( size_t iPcl = iPclStart ; iPcl < iPclEnd ; ++ iPcl )
    {   // For each particle in this slice...
        Vorton &    rVorton         = mVortons[ iPcl ] ;
        // Technically the baroclinic term should have density in the denominator,
        // but it's relatively expensive to calculate the local value, plus the
        // Boussinesq approximation assumes small density variations.
        // Also, when density variations are large, the interpolation
        // sometimes leads to non-physical artifacts like negative densities.
        // So instead, we use the ambient density in the denominator,
        // which yields the correct units and gets us in the right ballpark.
        // This is yet another example of where, for visual effects,
        // we take drastic liberties in the name of speed over accuracy.
        Vec3        densityGradient ;
        mDensityGradientGrid.Interpolate( densityGradient , rVorton.mPosition ) ;
        const Vec3 baroclinicGeneration = densityGradient ^ mGravAccel / mAmbientDensity;
        // The formula for line below is meant to update vorticity, but since
        // we store that as angular velocity, formula has an extra factor of 0.5.
        rVorton.mAngularVelocity += 0.5f * baroclinicGeneration * timeStep ;


Figure 4 shows a simulation with an initially motionless ball of heavy fluid, colored blue. The resulting motion looks like dye dropped into a glass of water and sinking, vaguely resembling the results of a Rayleigh-Taylor (RT) instability.

Note: The classic RT instability has (initially) nearly flat layers of fluid with different densities, which are in an unstable equilibrium. This droplet example is not really an example of the RT instability but the underlying cause of the RT instability is the same: fluid buoyancy.

Figure 4.Dye drop falling through fluid. Initially, the ball of fluid, which is heavier than the fluid around it, has no velocity. Then, it begins to fall and forms a vortex ring, leaving behind tendrils of dye.

Figure 5 shows two drops of fluid-one heavier (blue) and one lighter (red) than the surrounding fluid. The drops are initially motionless but soon start to move as a result of buoyancy. They form a pair of vortex rings that eventually collide.

Figure 5.Dye drops falling and rising through fluid. The heavier blue drop falls, the lighter red drop rises, and then they collide.

Performance profiles reveal that the fluid buoyancy computation, including particle-to-grid transfer, density gradient, and the baroclinic term calculation, uses only around 0.3 percent of the total time-three one-thousandths-which is nearly negligible. Typical durations for that computation, for these simulations, ran for only tens of microseconds per frame on even modest hardware like an Intel® Pentium® 4 processor running at 3.0 GHz, with significantly faster performance on an Intel® Core™2 Duo processor running at 2.6 GHz.

Coming Up

Future articles will build upon this installment, adding solid-body buoyancy, convection (thermal expansion and diffusion), and combustion (generating heat by chemical processes). These articles will combine for even more interesting and interactive effects, allowing game effects creators to let their users interact with their virtual worlds with even greater immersion.

Further Reading

  • Koumoutsakos, Cottet, & Rossinelli. (2008). Flow simulations using particles. (Note that their equation 67 has the wrong units for the baroclinic term, missing a in the denominator. They are likely assuming very small density variation and that the ambient density is 1.0 in whatever units their simulation uses.)

Related Articles

Fluid Simulation for Video Games (part 1)
Fluid Simulation for Video Games (part 2)
Fluid Simulation for Video Games (part 3)
Fluid Simulation for Video Games (part 4)
Fluid Simulation for Video Games (part 5)
Fluid Simulation for Video Games (part 6)
Fluid Simulation for Video Games (part 7)
Fluid Simulation for Video Games (part 8)
Fluid Simulation for Video Games (part 9)
Fluid Simulation for Video Games (part 10)
Fluid Simulation for Video Games (part 11)
Fluid Simulation for Video Games (part 12)
Fluid Simulation for Video Games (part 13)
Fluid Simulation for Video Games (part 14)
Fluid Simulation for Video Games (part 15)
Fluid Simulation for Video Games (part 16)
Fluid Simulation for Video Games (part 17)
Fluid Simulation for Video Games (part 18)
Fluid Simulation for Video Games (part 19)

About the Author

Dr. Michael J. Gourlay works as a Senior Software Engineer at Electronic Arts. He currently works as a senior lead software engineer on Madden NFL. He previously worked on the procedural animation system used by EA, and on Mixed Martial Arts (MMA). He was also a lead programmer on NASCAR. He architected the visual effects system used in EA games worldwide and patented algorithms for interactive, high-bandwidth online applications. He also teaches at the University of Central Florida (UCF) Florida Interactive Entertainment Academy (FIEA), an interdisciplinary graduate program that teaches programmers, producers and artists how to make video games and training simulations. Prior to joining EA, he performed scientific research using computational fluid dynamics(CFD) and the world's largest massively parallel supercomputers. His previous research also includes nonlinear dynamics in quantum mechanical systems, and atomic, molecular and optical physics. Michael received his degrees in physics and philosophy from Georgia Tech and the University of Colorado at Boulder.

For more complete information about compiler optimizations, see our Optimization Notice.



xinxin, as to your second observation about using a grid to mediate density:

You are right; one could directly compute density gradients using the particles.

For example using an SPH-like (which is to say, Monte-Carlo-like) approach. It just so happens that in a later pair of articles I do just that. Parts 15 and 16 present such an approach. As of writing this, Part 15 is available, but it is a preamble to Part 16, which applies that to the vortex particle method.

Furthermore, tracking the density jump is a topic for a future article, where the focus is on simulating liquids. Doing so entails tracking the liquid boundary, i.e. its surface.

You can expect to see more aritcles in the future that cover such topics.

Thanks for your interest and questions.

xinxin, thanks for your insightful questions.

You made two observations. I'll address them in separate comments. First, for the boundary condition:

The vorticity profile has a 1/r falloff asymptotically, so there is no finite cutoff. As you point out, combined with a strictly per-vortex approximation, that would not globally solve the BC. That is true regardless of how the simulation solves velocity from vorticity -- Poisson or not.

You can think of rigid bodies as an extension of the fluid, where its vorticity is simply twice the angular velocity. Any vortex particles that inside a rigid body should therefore have that vorticity.

You could therefore allow vortons to go anywhere in the domain, including inside rigid bodies. But as vortons enter rigid bodies, they will have the wrong vorticity. To resolve that you could assign the vorticity of any vorton inside rigid bodies, to the vorticity of the rigid body. To conserve angular momentum you would also have to adjust the angular momentum of the body to compensate for the change in angular momentum for that vorton.

If you take this approach, then due to vortex diffusion, it (eventually) solves the boundary condition you want to impose, namely no-slip.

This is (almost) the same approach that "penalty methods" take. The difference is that those methods do not immediately reassign vortex particles to have the vorticity of the bodies they enter; instead they gradually adjust vorticity to do so.

This resembles what my simulation does: It computes a target vorticity and only gradually brings each vorton to that value. Meanwhile, my approach also adjusts the body's angular momentum so that it is conserved.

My approach, however, takes one final step beyond this: It also ejects vortons from the body. (Penalty methods usually just leave vortons inside the rigid body. In principle, vortons should pervade the entire body, so they could contribute to the velocity field.) The upshot is that since, in my approach, vortons also carry density, ejecting vortons from rigid bodies satisfies the no-through condition.

This is a handy-waving argument that I meant to suggest that the approach has merit, for the problem it means to solve: Make a simulation that exhibits plausible fluid-like motion, while running fast. Does it converge to a physically correct solution? Almost certainly not, but I have not tried to validate this with any comparisons, nor would I consider the attempt to be worthwhile. I have taken so many other shortcuts and liberties that even if this approach solved the boundary conditions, many other shortcuts cause other deviations from reality.

That is the theme of this series of articles: Start by understanding physics and knowing about legitimate approaches, then take poetic license to create your own rules, and see if they work.

Let's parse "see if they work": In our context, the ultimate test for success is whether it looks /good/. Looking good, in an interactive simulation like video games, implies running fast, looking interesting, and not distracting the viewer with obvious absurdity.

I do admit, thought, that outside the context of these articles, a part of me is curious to quantify the error introduced by this approach. I suspect that my penalty-cum-projection approach could be made to converge to a proper solution, without sacrificing speed or simplicity. If it requires any change, it would be to the target vorticity.

Long story short, you are right: The BC solution is local, not global. But while some canonical solutions are gobal, the penalty method is purely local in the sense that it lets diffusion propagate the solution (so that it eventually becomes global).

sorry forget to say, very great and nice work. I could imagine how much effort had been put into this project and writings.

few comments so far, one thing, you are using vortex particles with a cut-off radius, I like this idea for hacking the vortex shedding process and no-through boundary conditions, because then each one vortex will cancel only one boundary velocity difference exactly and the strength is obtained straight forward(like we have a diagonal matrix), and then i am not sure, are you really using a Poisson solver to get velocity, or using cut-off kernel convolution? if it's a poisson solver, then things becomes dangerous, since it's global, then your BC handling strategy becomes incorrect. if using cut-off, it's fine.
Second thing, you spread and gather density using a grid, I think the grid will destroy all the turbulence that vortex buossinesq would bring to us, instead, I think directly track density in the space and construct surface normal(as if there is one density jump sheet) might bring way more complex visual results.

A question: Does this code (particularly the TBB) runs for MAC OSX?


Great articles and work!!!! Thank you for share it!

This article mentions the Boussinesq approximation and its shortcomings.

People interested in more details will want to read these articles and websites, which describe the rationale for these simplifications (namely, to eliminate sound waves, which cause problems for numerical simulations but which have negligible impact on flows much slower than the speed of sound) and alternatives to the Boussinesq approximation, which accomplish similar goals but with fewer limitations and anomalies:





Interesting thread on Reddit about these articles, including some good questions and elucidations:

Video of this buoyancy simulation: http://www.youtube.com/watch?v=5b2Fm0R3hGA

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