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NASA Scientific and Technical Aerospace Reports

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have improved the ability to monitor <strong>and</strong> predict transient movement of water <strong>and</strong> contaminants in the vadose. One of the<br />

advancements is the water flux meter developed by Pacific Northwest National Laboratory (PNNL). The water flux meter is<br />

a device that, when it is buried in the subsurface, measures the flux of water infiltrating from the surface. Direct measurement<br />

of this parameter is very useful since the flux to groundwater is generally estimated from rainfall data <strong>and</strong> assumptions related<br />

to transpiration by vegetation, runoff, <strong>and</strong> evaporation, <strong>and</strong> their seasonal variation. Four water flux meters were installed at<br />

the SRS to collect baseline data on the temporal variation in water flux. The flux meters were installed at locations with other<br />

vadose zone monitoring equipment to verify operation of various pieces of equipment <strong>and</strong> to prepare a more complete analysis<br />

of water flux in the vadose zone. The flux meters are currently in operation <strong>and</strong> collecting data.<br />

NTIS<br />

Flowmeters; Ground Water; Annual Variations; Contaminants<br />

20040111150 Lawrence Livermore National Lab., Livermore, CA<br />

Very High Resolution Simulations of Compressible, Turbulent Flows<br />

Woodward, P. R.; Porter, D. H.; Sytine, I.; Anderson, S. E.; Mirin, A. A.; Apr. 26, 2001; In English<br />

Report No.(s): DE2004-15005669; UCRL-JC-143626; No Copyright; Avail: National <strong>Technical</strong> Information Service (NTIS)<br />

The steadily increasing power of supercomputing systems is enabling very high resolution simulations of compressible,<br />

turbulent flows in the high Reynolds number limit, which is of interest in astrophysics as well as in several other fluid<br />

dynamical applications. This paper discusses two such simulations, using grids of up to 8 billion cells. In each type of flow,<br />

convergence in a statistical sense is observed as the mesh is refined. The behavior of the convergent sequences indicates how<br />

a subgrid-scale model of turbulence could improve the treatment of these flows by high-resolution Euler schemes like PPM.<br />

The best resolved case, a simulation of a Richtmyer-Meshkov mixing layer in a shock tube experiment, also points the way<br />

toward such a subgrid-scale model. Analysis of the results of that simulation indicates a proportionality relationship between<br />

the energy transfer rate from large to small motions <strong>and</strong> the determinant of the deviatoric symmetric strain as well as the<br />

divergence of the velocity for the large-scale field.<br />

NTIS<br />

Compressible Flow; Turbulence; Computerized Simulation<br />

20040111161 California Univ., Lawrence Berkeley National Lab., Berkeley, CA, USA<br />

Computational Economy Improvements in PRISM<br />

Tonse, S. R.; Brown, N. J.; 2004; 10 pp.; In English<br />

Report No.(s): DE2004-823936; No Copyright; Avail: Department of Energy Information Bridge<br />

The PRISM piecewise solution mapping procedure, in which the solution of the chemical kinetic ODE system is<br />

parameterized with quadratic polynomials, is applied to CFD simulations of H(sub 2)+air combustion. Initial cost of<br />

polynomial construction is expensive, but it is recouped as the polynomial is reused. We present two methods that help us to<br />

parameterize only in places that will ultimately have high reuse. We also implement non-orthogonal Gosset factorial designs,<br />

that reduce polynomial construction costs by a factor of two over previously used orthogonal factorial designs.<br />

NTIS<br />

Computational Fluid Dynamics; Combustion; Factorial Design<br />

20040111177 Lawrence Livermore National Lab., Livermore, CA<br />

Comparison of Direct Eulerian Godunov <strong>and</strong> Lagrange Plus Remap, Artificial Viscosity Schemes<br />

Pember, R. B.; Anderson, R. W.; Mar. 30, 2001; In English<br />

Report No.(s): DE2003-15005665; UCRL-JC-143206; No Copyright; Avail: National <strong>Technical</strong> Information Service (NTIS)<br />

The authors compare two algorithms for solving the equations of unsteady inviscid compressible flow in an Eulerian<br />

frame: a staggered grid, Lagrange plus remap artificial viscosity scheme <strong>and</strong> a cell-centered, direct Eulerian higher-order<br />

Godunov scheme. They use the two methods to compute solutions to a number of one- <strong>and</strong> two-dimensional problems. The<br />

results show the accuracy of the two schemes to be generally equivalent. In a 1984 survey paper by Woodward <strong>and</strong> Colella,<br />

the Lagrange plus remap approach did not compare favorably with the higher-order Godunov methodology. They examine,<br />

therefore, how certain features of the staggered grid scheme considered here contribute to its improved accuracy. The critical<br />

features are shown to be the use of a monotonic artificial viscosity in the Lagrange step <strong>and</strong>, in the remap step, the use of a<br />

corner transport upwind scheme with van Leer limiters in conjunction with separate advection of internal <strong>and</strong> kinetic energies.<br />

NTIS<br />

Viscosity; Algorithms; Compressible Flow; Computational Grids<br />

108

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