[3684] | 1 | !> @file user_flight.f90 |
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[2000] | 2 | !------------------------------------------------------------------------------! |
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[2696] | 3 | ! This file is part of the PALM model system. |
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[1957] | 4 | ! |
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[2000] | 5 | ! PALM is free software: you can redistribute it and/or modify it under the |
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| 6 | ! terms of the GNU General Public License as published by the Free Software |
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| 7 | ! Foundation, either version 3 of the License, or (at your option) any later |
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| 8 | ! version. |
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[1957] | 9 | ! |
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| 10 | ! PALM is distributed in the hope that it will be useful, but WITHOUT ANY |
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| 11 | ! WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR |
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| 12 | ! A PARTICULAR PURPOSE. See the GNU General Public License for more details. |
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| 13 | ! |
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| 14 | ! You should have received a copy of the GNU General Public License along with |
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| 15 | ! PALM. If not, see <http://www.gnu.org/licenses/>. |
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| 16 | ! |
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[3655] | 17 | ! Copyright 1997-2019 Leibniz Universitaet Hannover |
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[2000] | 18 | !------------------------------------------------------------------------------! |
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[1957] | 19 | ! |
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| 20 | ! Current revisions: |
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| 21 | ! ------------------ |
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| 22 | ! |
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[2001] | 23 | ! |
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[1957] | 24 | ! Former revisions: |
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| 25 | ! ----------------- |
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| 26 | ! $Id: user_flight.f90 3684 2019-01-20 20:20:58Z hellstea $ |
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[2716] | 27 | ! Corrected "Former revisions" section |
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| 28 | ! |
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| 29 | ! 2696 2017-12-14 17:12:51Z kanani |
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| 30 | ! Change in file header (GPL part) |
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[1957] | 31 | ! |
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[2716] | 32 | ! 2101 2017-01-05 16:42:31Z suehring |
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| 33 | ! |
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[2001] | 34 | ! 2000 2016-08-20 18:09:15Z knoop |
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| 35 | ! Forced header and separation lines into 80 columns |
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| 36 | ! |
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[1958] | 37 | ! 1957 2016-07-07 10:43:48Z suehring |
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| 38 | ! Initial revision |
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| 39 | ! |
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[1957] | 40 | ! Description: |
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| 41 | ! ------------ |
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| 42 | !> Calculation of user-defined output quantity for flight measurements after |
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| 43 | !> each timestep. |
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| 44 | !------------------------------------------------------------------------------! |
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| 45 | SUBROUTINE user_flight( var, id ) |
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| 46 | |
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| 47 | USE control_parameters |
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| 48 | |
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| 49 | USE grid_variables |
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| 50 | |
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| 51 | USE indices |
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| 52 | |
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| 53 | USE kinds |
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| 54 | |
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| 55 | USE user |
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| 56 | |
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| 57 | USE arrays_3d |
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| 58 | |
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| 59 | IMPLICIT NONE |
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| 60 | |
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| 61 | INTEGER(iwp) :: i !< index along x |
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| 62 | INTEGER(iwp) :: j !< index along y |
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| 63 | INTEGER(iwp) :: k !< index along z |
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| 64 | INTEGER(iwp) :: id !< variable identifyer, according to the settings in user_init_flight |
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| 65 | |
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| 66 | REAL(wp), DIMENSION(nzb:nzt+1,nysg:nyng,nxlg:nxrg) :: var !< treated variable |
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| 67 | |
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| 68 | ! |
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| 69 | !-- Here, the respective variable is calculated. There is no call of |
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| 70 | !-- exchange_horiz necessary. |
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| 71 | !-- The variable identifyer (id) must be set according to the settings in |
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| 72 | !-- user_init_flight. |
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| 73 | !-- Please note, so far, variable must be located at the center of a grid box. |
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| 74 | ! var = 0.0_wp |
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| 75 | |
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| 76 | ! SELECT CASE ( id ) |
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| 77 | ! |
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| 78 | ! CASE ( 1 ) |
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| 79 | ! DO i = nxl-1, nxr+1 |
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| 80 | ! DO j = nys-1, nyn+1 |
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| 81 | ! DO k = nzb, nzt |
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| 82 | ! var(k,j,i) = ABS( u(k,j,i ) |
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| 83 | ! ENDDO |
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| 84 | ! ENDDO |
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| 85 | ! ENDDO |
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| 86 | ! |
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| 87 | ! CASE ( 2 ) |
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| 88 | ! DO i = nxl-1, nxr+1 |
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| 89 | ! DO j = nys-1, nyn+1 |
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| 90 | ! DO k = nzb, nzt |
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| 91 | ! var(k,j,i) = ABS( v(k,j,i) ) |
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| 92 | ! ENDDO |
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| 93 | ! ENDDO |
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| 94 | ! ENDDO |
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| 95 | ! |
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| 96 | ! END SELECT |
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| 97 | |
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| 98 | |
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| 99 | END SUBROUTINE user_flight |
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