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VULCAN SPECIFICATIONS
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Hypersonic Airbreathing Propulsion Branch
Hypersonic Airbreathing Propulsion Branch


VULCAN: Roman God of the ForgeVULCAN, named for the Roman god of fire, is a Computational Fluid Dynamics software package (available for serial and parallel computational platforms) for turbulent reacting and non-reacting flows at conditions ranging from subsonic to hypersonic speeds. The computational cost of propulsion flow analysis is reduced through the use of special turbulent wall treatments, multi-grid methods for elliptic and space marching schemes, and conditioning of the governing equations to reduce numerical stiffness. Physical modeling capabilities are improved through the inclusion of models for compressibility, Reynolds stress anisotropies, turbulent diffusivity, finite rate chemistry, and turbulence/chemistry interaction effects. VULCAN can simulate two-dimensional, three-dimensional, or axi-symmetric problems on structured multi-block grid systems. A variety of PDE-based turbulence models are available (including explicit algebraic Reynolds stress models) for use with VULCAN. Hybrid Reynolds-Averaged Simulation / Large Eddy Simulation options are also present. VULCAN offers significant geometric flexibility; boundary conditions can be imposed on any boundary or boundary subset, and the code has (C0)continuous as well as non-C(0) continuous block-to-block interface capability. VULCAN also offers thermodynamic and kinetic model flexibility. The working fluid can be simulated as a calorically perfect single component gas, as a mixture of thermally perfect gases (with or without chemical reactions).


For a description of the current capabilities of VULCAN See:


CAPABILITIES SUMMARY TABLE

factorization
Multiple Unix and Linux platform support for either
     1) Block level parallelization using MPI or MPICH for multi-processor machines
     2) Serial execution for single CPU machines
2-D, axi-symmetric, or 3-D single or multi-block grid topologies
Block-to-block interface options:
     1) arbitrary, block face-to-block face C(0) continuous connectivity
     2) arbitrary, block face-to-block face non-C(0) continuous connectivity
Steady-state algorithms for spatially elliptic/hyperbolic and spatially
     parabolic/hyperbolic equations
     1) Runge-Kutta with implicit residual smoothing
     2) Diagonalized approximate factorization
     3) Incomplete LU (calorically perfect flows only)
Unsteady algorithms
     1) Runge-Kutta
     2) Diagonalized approximate with dual time-stepping
     3) Incomplete LU with dual time-stepping (calorically perfect flows only)
Convergence acceleration options:
     1) multigrid
     2) mesh sequencing
Gas models
     1) Single component calorically and thermally perfect gases
     2) Arbitrary multi-component mixtures of thermally perfect gases
Chemistry models
     1) Frozen flow
     2) Arbitrary, non-equilibrium, finite-rate chemical kinetics
Inviscid flux treatments
     1) Jameson's central differencing with artificial dissipation
     2) MUSCL kappa scheme of van Leer
          a) Roe's flux difference split scheme with entropy fixes
          b) Edwards' low dissipation flux split scheme
          c) HLLC scheme of Toro
Viscous flux treatments for laminar or turbulent flow
     1) Full Navier-Stokes
     2) Thin-layer Navier-Stokes
     3) Parabolized Navier-Stokes
Mean flow turbulence model options
     1) Spalart-Allmaras
     2) Wilcox k-omega (98)
     3) Wilcox low Reynolds no. k-omega (98)
     4) Menter k-omega (baseline)
     5) Menter k-omega (SST)
     6) Abid low Reynolds no. k-epsilon
     7) Gatski-Speziale EASM k-omega (98)
     8) Gatski-Speziale EASM k-epsilon
Mean flow turbulence boundary condition treatment options
     1) Wilcox compressible wall matching ( k-omega based models)
     2) Solve to wall (all models)
Hybrid RANS/LES options
     1) Detached Eddy Simulation (two-equation based model of Strelets)
     2) Hybrid RANS/LES model of Baurle and Edwards
Turbulence/chemistry interaction models
     1) Eddy break-up model of Magnussen and Hjertager
     2) Temperature fluctuations: average turbulent reaction rate coefficient
          a) Assumed gaussian probability density function (PDF)
          b) Assumed beta probability density function (PDF)
     3) Species fluctuations: average species product of concentration using a
          multi-variate assumed beta probability density function (PDF)


ONGOING EXTENSIONS

Highly Implicit algorithms
  • Incomplete LU extended to thermally perfect equation sets


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NASA Official Responsible For Content: Robert A. Baurle

This site's most recent update took place: 11/15/2010

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