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COSMO Sibiu 2013 Matthias Raschendorfer Towards a consolidated turbulence and surface coupling for COSMO and ICON: Technical issues preparing the common module for COSMO and ICON Revision of security limits and the problem with the stable boundary layer (SBL) Foreseen modifications within the first PT ConSAT
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Matthias RaschendorferCOSMO Sibiu 2013 DWD Some technical issues preparing the common module: Call of organize_turbdiff by a long parameter list Only one horizontal index of variable fields Extraction of horizontal operations from the turbulence code Horizontal shear; interpolations due to grid staggering Stronger modularization (common subroutines for turbdiff and turbtran) moist physics; turbulence model; initialization Removing obsolete parts of the code Different options for gaining positive definiteness of TKE, avoiding singularities in solution for stability functions and other security limits for future testing (stable boundary, SAT) Trying to generate a somehow more systematic logic of switches and options Requirement by ICON design More flexibility to adapt to hardware architecture Due to different horizontal ICON grid Clearer code structure; extensions easier to apply Facilitating future testing (SBL) More user friendly for testing procedure
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Matthias Raschendorfer DWD Treating implicit vertical diffusion as a part of the turbulence module Using a common subroutine for all species Including half-level variables (TKE) Including passive tracers Allowing treatment of non-gradient fluxes in the same framework Options for treatment of explicit tendencies Optional preconditioning Options for the treatment of the lower boundary (input of explicit surface fluxes possible) In case of surface tiles: flux aggregation (tile structure outside the turbdiff module so far) Diffusion of conserved variables and subsequent turbulent saturation adjustment possible Some technical issues preparing the common module: Easier exchange of complete turbulence/diffusion framework Code is much easier to handle; avoiding code repetitions Facilitates testing the effect of different numerical treatment Common tile structure not yet defined Easiest way to consider turbulent condensation in GS budgets COSMO Sibiu 2013 Forcing with prescribed surface fluxes possible Mainly present in ICON; a private test version with 2 horizontal indices exists Strategy: Generating interface for COSMO and using ICON-Module for further development!!
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The problem with the stable boundary layer (SBL): Matthias Raschendorfer DWD Almost no production term in a classical TKE equation vertical shear by the mean flow buoyancydissipation almost zero for low wind conditions negative for downward heat flux always a sink almost no vertical mixing even though it is usually present in nature complete decoupling of the surface almost no dissolution of fog and inversion layer clouds singularities in turbulence model model solution is strongly dependent on numerical details considerable problems with numerical stability CUS 2013
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Possible solutions of the problem: Matthias Raschendorfer DWD Introduction of artificial background mixing -minimal value of TKE -restriction of thermal stability - minimal value for turbulent diffusion coefficients (tkm[m,h]min) Problems with these measures -not physically based (except some additional l aminar diffusion) -often too much mixing in the lower nocturnal BL -either too fast or too slowly dissolution of inversion layer clouds -either too strong or too weak nocturnal temperature decrease at the surface -danger of smoothing out vertical jet structure (e.g. of the low level jet) Alternatives -Adopted numerical schemes -inherent vertical smoothing without explicit minimal diffusion coefficients -prognostic TKE equation guaranteeing positive definiteness without explicit limits CUS 2013 momentum scalars (heat) Ready in test version and ICON
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Matthias Raschendorfer DWD More physical based TKE and mixing in the stable BL -Additional TKE sources are already beneficial for EDR-forecast (for aviation) -Should be beneficial for near surface SBL as well. - Previous artificial security measures needs to be adopted! First candidate:the minimal diffusion coefficient -Previous value: tkv[h,m]min = 1.0 m 2 /s (same for scalars and momentum) -Seems to dissolve BL clouds much to early now (and was presumably always a bit too large) -Previous attempts to decrease it has not been successful. -After lots of general numerical improvement of the model and the introduction of the SSO-source term a further attempt has now been tried:New value: tkv[h,m]min = 0.4 m 2 /s CUS 2013 Physical based solution Introduction of additional turbulence production via scale interaction - thermal density circulations; wake production; horizontal shear Deardorff-reduction of the turbulent length scale Turbulent transport of turbulent scalar variances (TKESV) Considering circulation transport of GS and turbulent Considering turbulent condensation in GS budgets In official version; only wake production runs operational so far In official version; verification has been delayed In test version; needs to be introduced as an option verified against current development not yet implemented GS saturation adjustment needs to be substituted by statistical approach including turbulence ad convection
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15.11.2012 12 UTC
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Low level cloud cover CLCL RoutineExperiment s
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TKE/[m2/s2] diffusion-coefficient/[m2/s]: time-height cut all values are area averages RoutineExperiment
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Theta/[°C] Vel/[m/s] cloud-water-content/[Kg/Kg]: time-height cut RoutineExperiment all values are area averages
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Experiment - Routine before moister now moister before more TKE: Initiating cloud dissolution now more TKE (within the clouds) all values are area averages time-height cut
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vertical profile Routine Experiment all values are area averages now cooler day-time BL now much more BL clouds now more intense low level jet
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Matthias Raschendorfer DWD Conclusion: In the SBL pure turbulence would completely disappear, unless non-turbulent sub-grid processes are interacting. Introduction of scale interaction terms was the reason that previous security measures for the SBL could and must be degraded. Reduction of tkv[h,m]min diminishes excessive dissolution of inversion layer clouds that seemed to get increasingly worse lately and causes more BL clouds now. Less often completely wrong simulation of BL clouds cooler BL also during daytime => slightly negative BIAS of T2m_max we expect also less systematic radiative cooling of the soil during winter time (needs to be verified; experiment has been canceled due to technical problems) Reduction of tkv[h,m]min diminishes night-time heat transfer towards the soil. cooler clear sky surface layer during night => reduction of positive BIAS of T2m_min Operational at DWD since December 2012 CUS 2013
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Next steps: Matthias Raschendorfer DWD Investigation of the other security measures in the scheme CUS 2013 -Reformulation of the numerical sub schemes to allow for less restrictions (ready in a test version) -Less restrictive security measures to avoid singularities in the turbulent budget equations (ready in a test version) Further development of the scheme -Reformulation of the thermal circulation term into a thermal SSO-source term (prepared) -Implementation of missing circulation transport of GS and turbulent properties (additional non-gradient diffusion) -Reformulation of the surface-to-atmosphere transfer in order to be more sensitive for stable stratification (ConSAT) Testing/Adapting/Verification of various implementations -The not yet activated scale interaction terms (by convection and horizontal shear) (ready in official version) -Deardorff-restriction of turbulent length scale for stable stratification (ready in official version) -Turbulent transport of scalar variances (TKESV) (ready in test version; to be adapted to official code as an option) -Turbulent saturation adjustment in grid scale budgets (in principle already possible) Strategy: Generating interface for COSMO and using ICON-Module for further development!!
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Specific problems of SAT: CLM-Training Course The total effective vertical flux density can be written as: molecular diffusion coefficient effective velocity scale turbulent length scale It is squared surface area index pure turbulent velocity scale Above the laminar layer, where molecular diffusion is negligible and above the roughness layer it holds: only laminar diffusion at the surface Matthias Raschendorfer DWD Close to the surface 2 additional difficulties arise: -Laminar diffusion can’t be neglected -Roughness layer effects (SGS terms due to non-linearity of spatial differentiation): - form drag -effect of increased surface -modification of turbulent length scale earth roughness layer displace ment height rough ness length
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Vertical gradients increase significantly approaching the surface. Therefore the vertical profile of is not linear and can only be determined using further information. Integration yields: transfer layer resistance roughness layer resistance free atmospheric resistance specific roughness length The constant flux layer: In our model we assume that does not change significantly within the transfer layer between the surface and the lowest full model level. constant flux layer turbulent velocity scale Matthias Raschendorfer DWD CLM-Training Course squared surface area index
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laminar layer logarithmic Prandtl- layer profile unstable stable linear interpolated Prandtl layer roughness layer (expon. roughness- layer profile) lowest model main level upper boundary of the lowest model layer lower boundary of the lowest model layer SYNOP station lawn profile Mean GRID box profile Effective velocity scale profile turbulence- scheme no storage capacity Transfer scheme and 2m-values with respect to a SYNOP lawn: Exponential roughness layer profile is valid for the whole grid box, but it is not present at a SYNOP station from turbulence-scheme Matthias Raschendorfer DWD CLM-Training Course
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Calculation of the transport resistances: The current scheme in COSMO explicitly considers the roughness layer resistance for scalars: - applying and an effective SAI value for the whole roughness layer - using the laminar length scale and a proper scaling factor for scalars - assuming for, it can be written: The current scheme in COSMO explicitly considers the free atmospheric resistance: - applying a linear -profile between level(top of the roughness layer) and level (top of the lowest model layer) - using the atmospheric heightand the stability parameter it can be written: new branch Matthias Raschendorfer DWD May.2013 Can be expressed by surface layer variables only, increasing sensitivity on thermal stratification
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Investigation of numerical security limits in the related turbulence model Implementation, verification and documentation of the revised transfer formulation Detailed investigation of the problems with daily cycle of near surface variables using measurements and COSMO-SC Next steps: Matthias Raschendorfer DWD Extension of the profile function towards an universal one that includes the laminar limit, thus getting rid of using a virtual laminar layer. Revision of near surface diagnostics in particular with respect to their applicability at grid points with a large roughness length. Implementation of the vertically resolved roughness layer with roughness terms in all 1-st and second order budgets and considering only the not resolved part in the SAT scheme (reduction of roughness length). For longer terms: 1-st 1-year task COSMO Sibiu 2013
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contribution with pure turbulent profile function contribution for additional laminar correction pure neutral contribution analytically integrable dimensionless resistance and from TKE scheme The general valid resistance: COSMO Offenbach 2009 Matthias Raschendorfer lowest full level
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Normalized transition profile for wind speed: according classical measurements form Reichardt 1951 according approximation COSMO Offenbach 2009 Matthias Raschendorfer molecular solution turbulent solution
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filtered topography For any scale COSMO Matthias Raschendorfer Offenbach 2009
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earth roughness layer At the lowest level, where this is valid, it is: Roughness layer properties and the surface flux density: can be described in the roughness layer and von Kaman constant -surfaces normal to local turbulent and molecular flux densities, being a shifted topography without small scale modes not contributing to for any variable. Their area is times the horizontal projection displace ment height rough ness length CLM-Training Course mean distance form the rigid surface Using The flux densities of prognostic model variables at the lower model boundary are affected by the roughness layer and have turbulent as well as molecular contributions: The total effective vertical flux density can be written as: molecular diffusion coefficient effective velocity scale turbulent length scale It is squared surface area index pure turbulent velocity scale Above the laminar layer, where molecular diffusion is negligible and above the roughness layer it holds: only laminar diffusion at the surface Matthias Raschendorfer DWD Above the roughness layer, the surface area index is equal to 1 and can be chosen so that it holds there:
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Implicit calculation of surface temperature by liniarized surface energy budget, including a decoupled cover layer Vertically resolved roughness layer (interaction with roughness elements in budet equations) Further development of scale separation (namely related to convection and cloud processes) Consistent microphysics including SGS processes (turbulent and convective phase changes) Matthias Raschendorfer DWD Switching on the implemented scale interaction terms after verification against SYNOP data (operational verification) Reformulation of the surface induced density flow term (circulation term) in the current scheme to become a thermal SSO production dependent on SSO parameters Expression of direct sub grid scale transport by SSO eddies and horizontal shear eddies Introduction of an option for three additional prognostic scalar variance equations (UCTS) Further development: Detailed investigation of the problems with daily cycle of near surface variables using measurements and COSMO-SC (ConSAT) Implementation and verification of the full revised transfer formulation (ConSAT)
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