air-jet_fluent.jou.tpl

Optimus Fluent Gambit

;; **********************************************************
;; JET study
;; ----------------------------------------------------------
;; FLUENT JOURNAL FILE
;; ANTOINE DOZOLME ([e-mail])
;;
;; The values to be changed are the one just below the star line.
;; **********************************************************
;; Define here the reference value for the nusselt number:
;; must be equal to: 2*$r (m)
;; **********************************************************
/report/reference-values/length #R2#
;;****************************************
;; define here the reference temperature.
;; must be equal to the inlet temperature
;;****************************************
/report/reference-values/temperature 300
/file/read-case air-jet.msh
/define/models/axisymmetric yes
/define/models/energy yes no no no yes
/define/models/viscous/kw-sst yes
/define/operating-conditions/gravity yes 9.81 0
/define/boundary-conditions/velocity-inlet inlet
no
yes
yes
no
;;*************************************
;; the following line define the speed
;;*************************************
#Speed#
no
0
no
;;*************************
;; temperature at the inlet
;;*************************
300
no
yes
;;************************************
;; the following must be equal to 2*$r
;;************************************
#R2#
5
/define/boundary-conditions/pressure-inlet pres-inlet
no
0
no
0
no
300
no
yes
no
yes
;;****************************************
;; the following must be equal to 14*$r+$h
;;****************************************
#R14+H#
5
/define/boundary-conditions/wall wall
0
no
0
no
yes
temperature
no
;;*********************************************
;;define the wall temperature (k)
;;*********************************************
1000
no
no
0
0.5
/define/boundary-conditions/pressure-outlet outlet
no
0
no
300
no
yes
no
yes
;;****************************************
;;  the following must be equal to 8*$r+$h
;;****************************************
#R8+H#
5
/solve/init/init
/solve/iterate 1000000
wcd air-jet.gz

;;***************************************************************************
;;POSTPROCESSING COMMAND value will appear at the end of the jet.out file.
;;***************************************************************************
;;value of the integral of the enthalpy at the inlet
/report/surface-int inlet

total-enthalpy 
;;value of the Nusselt number on the wall
/report/surface-int wall

heat-flux

exit/y