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| 3 | <meta content="text/html; charset=windows-1252" http-equiv="CONTENT-TYPE"><title>PALM chapter 2.0</title> <meta content="StarOffice 7 (Win32)" name="GENERATOR"> <meta content="Marcus Oliver Letzel" name="AUTHOR"> <meta content="20040719;14534028" name="CREATED"> <meta content="20041117;10385730" name="CHANGED"> <meta content="parallel LES model" name="KEYWORDS"> <style> |
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| 4 | <!-- |
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| 5 | @page { size: 21cm 29.7cm } |
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| 7 | </style></head> |
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| 8 | |
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| 9 | <body style="direction: ltr;" lang="en-US"><h2 style="line-height: 100%;"><font size="4">2.0 |
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| 10 | Basic techniques of |
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| [5] | 11 | the LES model and its parallelization </font> |
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| [62] | 12 | </h2><p style="line-height: 100%;">LES models |
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| 13 | generally permit the |
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| [5] | 14 | simulation of turbulent flows, whereby those eddies, that carry the |
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| 15 | main energy are resolved by the numerical grid. Only the |
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| 16 | effect of such turbulence elements with diameter equal to or smaller |
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| 17 | than the grid spacing are parameterized in the model and |
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| 18 | by so-called subgrid-scale (SGS) transport. Larger structures are |
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| 19 | simulated directly (they are explicitly resolved) and their effects are |
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| 20 | represented by the advection terms. </p> |
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| [62] | 21 | <p style="font-style: normal; line-height: 100%;">PALM is |
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| 22 | based on the |
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| [5] | 23 | non-hydrostatic incompressible Boussinesq equations. It contains a |
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| 24 | water cycle with cloud formation and takes into account infrared |
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| 25 | radiative cooling in cloudy conditions. The model has six prognostic |
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| [62] | 26 | quantities in total – u,v,w, liquid water potential |
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| 27 | temperature |
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| 28 | <font face="Thorndale, serif">Θ</font><sub>l |
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| 29 | </sub>(BETTS, |
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| [5] | 30 | 1973), total water content q and subgrid-scale turbulent kinetic energy |
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| 31 | e. The |
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| 32 | subgrid-scale turbulence is modeled according to DEARDOFF (1980) and |
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| 33 | requires the solution of an additional prognostic equation for the |
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| 34 | turbulent kinetic energy e. The long wave radiation scheme is based |
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| 35 | on the parametrization of cloud effective emissivity (e.g. Cox, 1976) |
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| 36 | and condensation is considered by a simple '0%-or-100%'-scheme, which |
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| 37 | assumes that within each grid box the air is either entirely |
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| 38 | unsaturated or entirely saturated ( see e.g., CUIJPERS and DUYNKERKE, |
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| 39 | 1993). The water cycle is closed by using a simplified version of |
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| 40 | KESSLERs scheme (KESSLER, 1965; 1969) to parameterize precipitation |
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| [62] | 41 | processes (MÜLLER and CHLOND, 1996). Incompressibility is |
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| [5] | 42 | applied by means of a Poisson equation for pressure, which is solved |
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| 43 | with a direct method (SCHUMANN and SWEET, 1988). The Poisson equation |
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| 44 | is Fourier transformed in both horizontal directions and the |
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| 45 | resulting tridiagonal matrix is solved for the transformed pressure |
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| 46 | which is then transformed back. Alternatively, a multigrid method can |
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| 47 | also be used. Lateral boundary conditions of the model are cyclic and |
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| 48 | MONIN-OBUKHOV similarity is assumed between the surface and the first |
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| 49 | computational grid level above. Alternatively, noncyclic boundary |
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| 50 | conditions |
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| 51 | (Dirichlet/Neumann) can be used along one of the |
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| 52 | horizontal directions. At the lower surface, either temperature/ |
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| 53 | humidity or their respective fluxes can be prescribed. </p> |
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| [62] | 54 | <p style="font-style: normal; line-height: 100%;">The |
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| 55 | advection terms |
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| [5] | 56 | are treated by the scheme proposed by PIACSEK and WILLIAMS (1970), |
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| 57 | which conserves the integral of linear and quadratic quantities up to |
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| 58 | very small errors. The advection of scalar quantities can optionally |
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| 59 | be performed by the monotone, locally modified version of Botts |
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| 60 | advection scheme (CHLOND, 1994). The time integration is performed |
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| 61 | with the third-order Runge-Kutta scheme. A second-order Runge-Kutta |
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| 62 | scheme, a leapfrog scheme and an Euler scheme are also implemented.</p> |
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| [62] | 63 | <p style="line-height: 100%;">By default, the time step is |
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| 64 | computed |
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| [5] | 65 | with respect to the different criteria (CFL, diffusion) and adapted |
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| 66 | automatically. In case of a non-zero geostrophic |
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| 67 | wind the coordinate system can be moved along with the mean wind in |
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| 68 | order to maximize the time step (Galilei-Transformation). </p> |
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| [62] | 69 | <p style="font-style: normal; line-height: 100%;">In |
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| 70 | principle a model |
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| [5] | 71 | run is carried out in the following way: After reading the control |
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| 72 | parameters given by the user, all prognostic variables are |
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| 73 | initialized. Initial values can be e.g. vertical profiles of the |
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| 74 | horizontal wind, calculated using a 1D subset of the 3D prognostic |
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| 75 | equation and are set in the 3D-Model as horizontally homogeneous |
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| 76 | initial values. Temperature profiles can only be prescribed linear |
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| 77 | (with constant gradients, which may change for different vertical |
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| 78 | height intervals) and they are assumed in the 1D-Model as stationary. |
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| 79 | After the initialization phase during which also different kinds of |
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| 80 | disturbances may be imposed to the prognostic fields, the time |
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| 81 | integration begins. Here for each individual time step the prognostic |
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| 82 | equations are successively solved for the velocity components u, v and |
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| 83 | w |
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| 84 | as well as for the potential temperature and possibly for the TKE. |
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| 85 | After the calculation of the boundary values in accordance with the |
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| 86 | given boundary conditions the provisional velocity fields are |
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| 87 | corrected with the help of the pressure solver. Following this, all |
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| 88 | diagnostic turbulence quantities including possible |
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| [62] | 89 | Prandtl-layer–quantities are computed. At the end of a time |
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| [5] | 90 | step the data output requested by the user is made |
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| 91 | (e.g. statistic of analyses for control purposes or profiles and/or |
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| 92 | graphics data). If the given end-time was reached, binary data maybe |
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| 93 | be saved for restart. </p> |
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| [62] | 94 | <p style="font-style: normal; line-height: 100%;">The |
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| 95 | model is based |
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| [5] | 96 | on the originally non-parallel LES model which has been operated at the |
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| 97 | institute since 1989 |
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| 98 | and which was parallelized for massively parallel computers with |
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| 99 | distributed memory using the Message-Passing-Standard MPI. It is |
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| 100 | still applicable on a single processor and also well optimized for |
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| 101 | vector machines. The parallelization takes place via a so-called domain |
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| 102 | decomposition, which divides the entire model |
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| 103 | domain into individual, vertically standing cubes, which extend from |
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| 104 | the bottom to the top of the model domain. One processor (processing |
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| 105 | element, PE) is assigned to each cube, which |
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| 106 | accomplishes the computations on all grid points of the subdomain. |
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| 107 | Users can choose between a two- and a one-dimensional domain |
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| 108 | decomposition. A 1D-decomposition is preferred on machines with a |
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| [62] | 109 | slow network interconnection. In case of a 1D-decomposition, |
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| 110 | the |
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| [5] | 111 | grid points along x direction are |
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| 112 | distributed among the individual processors, but in y- and z-direction |
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| 113 | all respective grid points belong to the same PE. </p> |
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| [62] | 114 | <p style="line-height: 100%;">The calculation of central |
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| 115 | differences or |
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| [5] | 116 | non-local arithmetic operations (e.g. global |
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| 117 | sums, FFT) demands communication and an appropriate data exchange |
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| 118 | between the PEs. As a substantial innovation in relation to |
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| 119 | the non-parallel model version the individual subdomains are |
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| 120 | surrounded by so-called ghost points, which contain the grid point |
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| 121 | information of the neighbor processors. The appropriate grid point |
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| 122 | values must be exchanged after each change (i.e. in particular after |
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| 123 | each time step). For this purpose MPI routines (<tt>MPI_SENDRCV</tt>) |
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| 124 | are used. For the solution of the FFT conventional (non-parallelized) |
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| 125 | procedures are used. Given that the FFTs are used in x and/or |
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| 126 | y-direction, the data which lie distributed on the individual central |
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| 127 | processing elements, have to be collected and/or relocated before. |
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| [62] | 128 | This happens by means of the routine <tt>MPI_ALLTOALLV</tt>. |
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| 129 | Certain |
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| [5] | 130 | global operations like e.g. the search for absolute maxima or minima |
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| 131 | within the 3D-arrays likewise require the employment of special MPI |
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| 132 | routines (<tt>MPI_ALLREDUCE</tt>). </p> |
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| [62] | 133 | <p style="line-height: 100%;">Further details of the |
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| 134 | internal model |
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| [5] | 135 | structure are described in the <a href="../tec/index.html">technical/numerical |
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| 136 | documentation</a>. <br> |
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| 137 | </p> |
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| [62] | 138 | <hr><font color="#000080"><font color="#000080"><br><a href="chapter_1.0.html"><font color="#000080"><img name="Grafik1" src="left.gif" align="bottom" border="2" height="32" width="32"></font></a><a href="index.html"><font color="#000080"><img name="Grafik2" src="up.gif" align="bottom" border="2" height="32" width="32"></font></a><a href="chapter_3.0.html"><font color="#000080"><img name="Grafik3" src="right.gif" align="bottom" border="2" height="32" width="32"></font></a><br> |
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| 139 | </font></font><br><p style="line-height: 100%;"><span style="font-style: italic;">Last |
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| 140 | change: </span>$Id: chapter_2.0.html 62 2007-03-13 02:52:40Z gronemeier $<font color="#000080"><font color="#000080"><br> |
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| 141 | </font></font></p></body></html> |
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