CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > Siemens

Drmast Subroutine

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   September 6, 2014, 05:19
Default Drmast Subroutine
  #1
New Member
 
Join Date: Sep 2014
Posts: 1
Rep Power: 0
Hobos is on a distinguished road
Dear Colleagues,

I am trying to simulate and compare the mass and heat transfer using drmast and drheat subroutines against the standard mass and heat transfer. I have used some of the equations in the user subroutines provided in star and the methodology and some from YAWS. But so far, I am only able to run the subroutines at droplet temp of 293K but not for temperatures higher than 293K.

Have I done anything wrong?

Please help and I look forward to hearing from you.

Regards,

Hobos

CC GAS CONSTANT (UGC)
UGC=8313
PI=3.1415927
CC MOLECULAR WEIGHT OF AIR OF WHICH N2 WAS ASSUMED
WTMOLN=28.96
CC MOLECULAR WEIGHT OF PENTANE
WTMOL=72
CC - MEAN TEMPERATURE OF FILM (TF)
TF=(T+TD)*0.5
CC================================================ =======================
CC PROPERIES OF AIR
CC================================================ =======================
CC - VISCOSITY AT TEMPERATURE TF (YAWS)
AVA=4.4656
BVA=6.3814E-1
CVA=-2.6596E-4
DVA=5.4113E-8
EQA1=AVA+(BVA*TF)+(CVA*(TF**2))+(DVA*(TF**3))
VISAL=EQA1*1E-3
CC - SPECIFIC HEAT AT CONSTANT PRESSURE AND AT TEMPERATURE TF (YAWS)
ASHA=28.7168
BSHA=7.3458E-3
CSHA=-4.5476E-5
DSHA=1.1641E-7
ESHA=-1.2246E-10
FSHA=5.9045E-14
GSHA=-1.0875E-17
EQA2=ASHA+(BSHA*TF)+(CSHA*(TF**2))+(DSHA*(TF**3))+ (ESHA*(TF**4))
EQA3=EQA2+(FSHA*(TF**5))+(GSHA*(TF**6))
SHAP=EQA3/(WTMOLN*1.0E-3)
CC - THERMAL CONDUCTIVITY (YAWS)
ATCA=-2.2678E-4
BTCA=1.0275E-4
CTCA=-6.0151E-8
DCTA=2.2332E-11
TCA=ATCA+(BTCA*TF)+(CTCA*(TF**2))+(DCTA*(TF**3))
CC================================================ =======================
CC PROPERTIES OF VAPOUR -> PENTANE FUEL
CC================================================ =======================
CC - VISCOSITY (YAWS)
AVV=-3.2016
BVV=0.2675
CVV=-6.6178E-5
EQV1=AVV+(BVV*TF)+(CVV*(TF**2))
VISV=EQV1*1E-3
CC - SPECIFIC HEAT AT CONSTANT PRESSURE AT MEAN TEMPERATURE (YAWS)
ASHV=26.671
BSHV=0.32324
CSHV=4.282E-5
DSHV=-1.664E-7
ESHV=5.6036E-11
EQV2=ASHV+(BSHV*TF)+(CSHV*(TF**2))+(DSHV*(TF**3))+ (ESHV*. (TF**4))
CPVPM=EQV2/(WTMOL*1.0E-3)
CC - THERMAL CONDUCTIVITY (YAWS)
ATCV=-0.00137
BTCV=1.8081E-5
CTCV=1.2136E-8
TCV=ATCV+(BTCV*TF)+(CTCV*(TF**2))
CC================================================ =======================
CC PROPERTIES OF LIQUID -> PENTANE FUEL
CC================================================ =======================
C.....COEFFICENTS OF ALHV,CLHV,NLHV, FOR PENTANE LATENT HEAT (YAWS)
ALHV=39.8543
CLHV=469.65
NLHV=0.398
C.....LATENT HEAT VAPOURIZATION IN kJ/mol
EQ4=(1-(TD/CLHV))**NLHV
LHV=ALHV*EQ4
C.....LATENT HEAT IN J/kg
HV=(LHV*1000)/(WTMOL*1.0E-3)
C....COEFFICENTS OF ASP,BSP,CSP,DSP,FSP, FOR PENTANE SATURATION PRESSURE
ASP=33.324
BSP=-2422.7
CSP=-9.2354
DSP=9.0199E-11
FSP=4.105E-6
C.....SATURATION PRESSURE IN MM Hg (YAWS)
EQ5=ASP+(BSP/TD)+(CSP*LOG10(TD))+(DSP*TD)+(FSP*(TD**2))
SP=10**EQ5
C.....SURAFCE HEAT IN Pa
PS=SP*133.322365
CC================================================ =======================
CC PROPERTIES OF VAPOUR-GAS MIXTURE IN FILM NEXT TO LIQUID SURFACE
CC================================================ =======================
CC - FILM MOLECUAR WEIGHT (WF)
C MOLE FRACTION OF VAPOUR
PF=PS/P
C. MOLE FRACTION OF AIR
OMPF=1-PF
C. MASS FRACTION OF FILM
WF=(OMPF*WG)+(PF*WP)
CC - FILM GAS CONSTANT
VGFGC=UGC/WF
CC - FILM VISCOSITY (VF)
VISF=(OMPF*VISAL)+(PF*VISV)
CC - FILM THERMAL CONDUCTIVITY (TCF)
TCF=(OMPF*TCA)+(PF*TCV)
CC - SPECIFIC HEAT AT CONSTANT PRESSURE (SHFP)
SHFP=((OMPF*WG*SHAP)+(PF*WP*CPVPM))/WF
CC - MASS DIFFUSION COEFFICIENT OF PENTANE LIQUID-GAS MIXTURE (YAWS)
AD=-0.073984
BD=0.000401868
CD=4.34982E-7
DCM=(AD+(BD*TF)+(CD*(TF**2)))*0.0001
CC================================================ =======================
CC CHARACTERISTIC NUMBERS
CC================================================ =======================
CC - RELATIVE VELOCITY
VR=SQRT(((U-UD)**2)+((V-VD)**2)+((W-WD)**2))
CC - REYNOLDS NUMBER
RE=(DEN*VR*DRD)/VISF
SQRE=SQRT(RE)
CC - PRANDTL NUMBER
PR=(SHFP*VISF)/TCF
CC - NUSSELT NUMBER
ANU=2+(0.6*SQRE*(PR**0.3333))
CC - SCHMIDT NUMBER
SCT=VISF/(DEN*DCM)
CC - SHERWOOD NUMBER
SH =2+(0.6*SQRE*(SCT**0.3333))
CC================================================ =======================
CC EVAPORATED MASS
CC================================================ =======================
CC - TRANSFER COEFFICIENT OF MASS
TCM=SH*DCM/(TF*VGFGC*DRD)
CC - PARTIAL PRESSURE OF THE VAPOUR IN THE BULK GAS
PV=(F*P*WG)/WP
CC - EVAPORATED MASS PER SECOND
A=PI*(DRD**2)
EM=(A*TCM*P)*(LOG((P-PV)/(P-PS)))
CC-------------------------------------------------------------------------
RETURN
Hobos is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Error in subroutine CONVERT_NAME_U2S_INT JDQFD CFX 2 January 21, 2014 09:19
Fortran Subroutine Error sergiorbrett CFX 12 September 3, 2012 07:40
Errorin subroutine appeared when applying cavitation model pitisrisuk CFX 1 July 2, 2012 03:36
FIDAP subroutine: USRBDY Shuwen Tzeng FLUENT 0 September 3, 2004 03:40
Trouble in using subroutine (FIDAP) Sindy FLUENT 0 July 5, 2004 07:07


All times are GMT -4. The time now is 20:22.