TALK=T;RUN(1,1)
DISPLAY
This case concerns two-dimensional, incompressible flow across
a non-symmetric, 10% thick conventional aerofoil (referred to
as the "Model A-airfoil"). The angle of attack is 0 degrees.
The trailing edge is modified slightly from the original
definition such that the aerofoil closes at chord=1 to give
a sharp trailing edge.
Calculations are made with the high-Re form of the
Spalart-Allmaras model, using wall functions.
ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(S-A Model-A Airfoil )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 0
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 241
XULAST =6.
XFRAC(1)=0.036988 ;XFRAC(2)=0.070613
XFRAC(3)=0.101181 ;XFRAC(4)=0.12897
XFRAC(5)=0.154233 ;XFRAC(6)=0.1772
XFRAC(7)=0.198078 ;XFRAC(8)=0.217059
XFRAC(9)=0.234314 ;XFRAC(10)=0.25
XFRAC(11)=0.264924 ;XFRAC(12)=0.278492
XFRAC(13)=0.290826 ;XFRAC(14)=0.302039
XFRAC(15)=0.312232 ;XFRAC(16)=0.321499
XFRAC(17)=0.329924 ;XFRAC(18)=0.337582
XFRAC(19)=0.344544 ;XFRAC(20)=0.350874
XFRAC(21)=0.356628 ;XFRAC(22)=0.361858
XFRAC(23)=0.366614 ;XFRAC(24)=0.370937
XFRAC(25)=0.374867 ;XFRAC(26)=0.37844
XFRAC(27)=0.381688 ;XFRAC(28)=0.38464
XFRAC(29)=0.387325 ;XFRAC(30)=0.389765
XFRAC(31)=0.391983 ;XFRAC(32)=0.394
XFRAC(33)=0.395833 ;XFRAC(34)=0.397425
XFRAC(35)=0.398942 ;XFRAC(36)=0.400386
XFRAC(37)=0.401761 ;XFRAC(38)=0.403071
XFRAC(39)=0.404318 ;XFRAC(40)=0.405507
XFRAC(41)=0.406638 ;XFRAC(42)=0.407716
XFRAC(43)=0.408742 ;XFRAC(44)=0.409719
XFRAC(45)=0.41065 ;XFRAC(46)=0.411537
XFRAC(47)=0.412381 ;XFRAC(48)=0.413185
XFRAC(49)=0.413951 ;XFRAC(50)=0.41468
XFRAC(51)=0.415375 ;XFRAC(52)=0.416037
XFRAC(53)=0.416667 ;XFRAC(54)=0.417297
XFRAC(55)=0.417958 ;XFRAC(56)=0.418653
XFRAC(57)=0.419382 ;XFRAC(58)=0.420148
XFRAC(59)=0.420952 ;XFRAC(60)=0.421797
XFRAC(61)=0.422683 ;XFRAC(62)=0.423614
XFRAC(63)=0.424591 ;XFRAC(64)=0.425618
XFRAC(65)=0.426695 ;XFRAC(66)=0.427827
XFRAC(67)=0.429015 ;XFRAC(68)=0.430262
XFRAC(69)=0.431572 ;XFRAC(70)=0.432947
XFRAC(71)=0.434392 ;XFRAC(72)=0.435908
XFRAC(73)=0.4375 ;XFRAC(74)=0.438997
XFRAC(75)=0.44051 ;XFRAC(76)=0.442037
XFRAC(77)=0.44358 ;XFRAC(78)=0.445138
XFRAC(79)=0.446711 ;XFRAC(80)=0.448301
XFRAC(81)=0.449906 ;XFRAC(82)=0.451527
XFRAC(83)=0.453165 ;XFRAC(84)=0.454819
XFRAC(85)=0.45649 ;XFRAC(86)=0.458177
XFRAC(87)=0.459881 ;XFRAC(88)=0.461602
XFRAC(89)=0.46334 ;XFRAC(90)=0.465096
XFRAC(91)=0.466869 ;XFRAC(92)=0.46866
XFRAC(93)=0.470469 ;XFRAC(94)=0.472296
XFRAC(95)=0.474141 ;XFRAC(96)=0.476005
XFRAC(97)=0.477887 ;XFRAC(98)=0.479788
XFRAC(99)=0.481709 ;XFRAC(100)=0.483648
XFRAC(101)=0.485607 ;XFRAC(102)=0.487585
XFRAC(103)=0.489583 ;XFRAC(104)=0.491581
XFRAC(105)=0.49356 ;XFRAC(106)=0.495519
XFRAC(107)=0.497458 ;XFRAC(108)=0.499378
XFRAC(109)=0.501279 ;XFRAC(110)=0.503162
XFRAC(111)=0.505025 ;XFRAC(112)=0.506871
XFRAC(113)=0.508698 ;XFRAC(114)=0.510507
XFRAC(115)=0.512298 ;XFRAC(116)=0.514071
XFRAC(117)=0.515827 ;XFRAC(118)=0.517565
XFRAC(119)=0.519286 ;XFRAC(120)=0.52099
XFRAC(121)=0.522677 ;XFRAC(122)=0.524348
XFRAC(123)=0.526002 ;XFRAC(124)=0.527639
XFRAC(125)=0.529261 ;XFRAC(126)=0.530866
XFRAC(127)=0.532455 ;XFRAC(128)=0.534029
XFRAC(129)=0.535587 ;XFRAC(130)=0.53713
XFRAC(131)=0.538657 ;XFRAC(132)=0.540169
XFRAC(133)=0.541667 ;XFRAC(134)=0.543301
XFRAC(135)=0.544903 ;XFRAC(136)=0.546473
XFRAC(137)=0.548013 ;XFRAC(138)=0.549523
XFRAC(139)=0.551003 ;XFRAC(140)=0.552454
XFRAC(141)=0.553877 ;XFRAC(142)=0.555271
XFRAC(143)=0.556638 ;XFRAC(144)=0.557979
XFRAC(145)=0.559293 ;XFRAC(146)=0.560582
XFRAC(147)=0.561845 ;XFRAC(148)=0.563083
XFRAC(149)=0.564297 ;XFRAC(150)=0.565488
XFRAC(151)=0.566655 ;XFRAC(152)=0.567799
XFRAC(153)=0.568921 ;XFRAC(154)=0.57002
XFRAC(155)=0.571098 ;XFRAC(156)=0.572155
XFRAC(157)=0.573192 ;XFRAC(158)=0.574208
XFRAC(159)=0.575204 ;XFRAC(160)=0.57618
XFRAC(161)=0.577137 ;XFRAC(162)=0.578076
XFRAC(163)=0.578996 ;XFRAC(164)=0.579898
XFRAC(165)=0.580783 ;XFRAC(166)=0.58165
XFRAC(167)=0.5825 ;XFRAC(168)=0.583333
XFRAC(169)=0.584023 ;XFRAC(170)=0.584727
XFRAC(171)=0.585444 ;XFRAC(172)=0.586177
XFRAC(173)=0.586923 ;XFRAC(174)=0.587685
XFRAC(175)=0.588462 ;XFRAC(176)=0.589254
XFRAC(177)=0.590062 ;XFRAC(178)=0.590887
XFRAC(179)=0.591728 ;XFRAC(180)=0.592585
XFRAC(181)=0.59346 ;XFRAC(182)=0.594353
XFRAC(183)=0.595263 ;XFRAC(184)=0.596191
XFRAC(185)=0.597138 ;XFRAC(186)=0.598104
XFRAC(187)=0.599089 ;XFRAC(188)=0.600094
XFRAC(189)=0.601119 ;XFRAC(190)=0.602165
XFRAC(191)=0.603231 ;XFRAC(192)=0.604319
XFRAC(193)=0.605429 ;XFRAC(194)=0.60656
XFRAC(195)=0.607715 ;XFRAC(196)=0.608892
XFRAC(197)=0.610093 ;XFRAC(198)=0.611318
XFRAC(199)=0.612568 ;XFRAC(200)=0.613842
XFRAC(201)=0.615142 ;XFRAC(202)=0.616468
XFRAC(203)=0.617821 ;XFRAC(204)=0.6192
XFRAC(205)=0.620607 ;XFRAC(206)=0.622043
XFRAC(207)=0.623507 ;XFRAC(208)=0.625
XFRAC(209)=0.626699 ;XFRAC(210)=0.628568
XFRAC(211)=0.630624 ;XFRAC(212)=0.632886
XFRAC(213)=0.635373 ;XFRAC(214)=0.63811
XFRAC(215)=0.64112 ;XFRAC(216)=0.644431
XFRAC(217)=0.648073 ;XFRAC(218)=0.652079
XFRAC(219)=0.656486 ;XFRAC(220)=0.661334
XFRAC(221)=0.666667 ;XFRAC(222)=0.672803
XFRAC(223)=0.679554 ;XFRAC(224)=0.686979
XFRAC(225)=0.695147 ;XFRAC(226)=0.704132
XFRAC(227)=0.714015 ;XFRAC(228)=0.724887
XFRAC(229)=0.736845 ;XFRAC(230)=0.75
XFRAC(231)=0.763491 ;XFRAC(232)=0.778331
XFRAC(233)=0.794655 ;XFRAC(234)=0.812611
XFRAC(235)=0.832363 ;XFRAC(236)=0.85409
XFRAC(237)=0.877989 ;XFRAC(238)=0.904279
XFRAC(239)=0.933198 ;XFRAC(240)=0.965008
XFRAC(241)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 139
YVLAST =5.
YFRAC(1)=0.045029 ;YFRAC(2)=0.085964
YFRAC(3)=0.123178 ;YFRAC(4)=0.157009
YFRAC(5)=0.187764 ;YFRAC(6)=0.215723
YFRAC(7)=0.241141 ;YFRAC(8)=0.264247
YFRAC(9)=0.285254 ;YFRAC(10)=0.30435
YFRAC(11)=0.321711 ;YFRAC(12)=0.337493
YFRAC(13)=0.351841 ;YFRAC(14)=0.364884
YFRAC(15)=0.376741 ;YFRAC(16)=0.387521
YFRAC(17)=0.39732 ;YFRAC(18)=0.406229
YFRAC(19)=0.414328 ;YFRAC(20)=0.42169
YFRAC(21)=0.428384 ;YFRAC(22)=0.434468
YFRAC(23)=0.44 ;YFRAC(24)=0.445119
YFRAC(25)=0.449773 ;YFRAC(26)=0.454004
YFRAC(27)=0.45785 ;YFRAC(28)=0.461346
YFRAC(29)=0.464525 ;YFRAC(30)=0.467415
YFRAC(31)=0.470042 ;YFRAC(32)=0.47243
YFRAC(33)=0.474601 ;YFRAC(34)=0.476575
YFRAC(35)=0.478369 ;YFRAC(36)=0.48
YFRAC(37)=0.481613 ;YFRAC(38)=0.48315
YFRAC(39)=0.484613 ;YFRAC(40)=0.486006
YFRAC(41)=0.487333 ;YFRAC(42)=0.488597
YFRAC(43)=0.489801 ;YFRAC(44)=0.490947
YFRAC(45)=0.492039 ;YFRAC(46)=0.493079
YFRAC(47)=0.49407 ;YFRAC(48)=0.495013
YFRAC(49)=0.495911 ;YFRAC(50)=0.496766
YFRAC(51)=0.497581 ;YFRAC(52)=0.498357
YFRAC(53)=0.499096 ;YFRAC(54)=0.4998
YFRAC(55)=0.500518 ;YFRAC(56)=0.501227
YFRAC(57)=0.501927 ;YFRAC(58)=0.502619
YFRAC(59)=0.503303 ;YFRAC(60)=0.503979
YFRAC(61)=0.504646 ;YFRAC(62)=0.505306
YFRAC(63)=0.505957 ;YFRAC(64)=0.506601
YFRAC(65)=0.507237 ;YFRAC(66)=0.507865
YFRAC(67)=0.508486 ;YFRAC(68)=0.509099
YFRAC(69)=0.509705 ;YFRAC(70)=0.510304
YFRAC(71)=0.510896 ;YFRAC(72)=0.511495
YFRAC(73)=0.512101 ;YFRAC(74)=0.512714
YFRAC(75)=0.513335 ;YFRAC(76)=0.513963
YFRAC(77)=0.514599 ;YFRAC(78)=0.515243
YFRAC(79)=0.515894 ;YFRAC(80)=0.516554
YFRAC(81)=0.517221 ;YFRAC(82)=0.517897
YFRAC(83)=0.518581 ;YFRAC(84)=0.519273
YFRAC(85)=0.519973 ;YFRAC(86)=0.520682
YFRAC(87)=0.5214 ;YFRAC(88)=0.522186
YFRAC(89)=0.523012 ;YFRAC(90)=0.523879
YFRAC(91)=0.524789 ;YFRAC(92)=0.525744
YFRAC(93)=0.526748 ;YFRAC(94)=0.527801
YFRAC(95)=0.528908 ;YFRAC(96)=0.530069
YFRAC(97)=0.531289 ;YFRAC(98)=0.53257
YFRAC(99)=0.533914 ;YFRAC(100)=0.535326
YFRAC(101)=0.536809 ;YFRAC(102)=0.538366
YFRAC(103)=0.54 ;YFRAC(104)=0.541749
YFRAC(105)=0.543673 ;YFRAC(106)=0.545789
YFRAC(107)=0.548117 ;YFRAC(108)=0.550677
YFRAC(109)=0.553494 ;YFRAC(110)=0.556592
YFRAC(111)=0.56 ;YFRAC(112)=0.563278
YFRAC(113)=0.566885 ;YFRAC(114)=0.570852
YFRAC(115)=0.575215 ;YFRAC(116)=0.580015
YFRAC(117)=0.585295 ;YFRAC(118)=0.591103
YFRAC(119)=0.597492 ;YFRAC(120)=0.60452
YFRAC(121)=0.61225 ;YFRAC(122)=0.620753
YFRAC(123)=0.630107 ;YFRAC(124)=0.640396
YFRAC(125)=0.651715 ;YFRAC(126)=0.664164
YFRAC(127)=0.677859 ;YFRAC(128)=0.692924
YFRAC(129)=0.709494 ;YFRAC(130)=0.727722
YFRAC(131)=0.747773 ;YFRAC(132)=0.769829
YFRAC(133)=0.79409 ;YFRAC(134)=0.820778
YFRAC(135)=0.850134 ;YFRAC(136)=0.882425
YFRAC(137)=0.917946 ;YFRAC(138)=0.95702
YFRAC(139)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 1
ZWLAST =1.
ZFRAC(1)=1.
************************************************************
Group 6. Body-Fitted Coordinates
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(1)=P1 ;NAME(3)=U1
NAME(5)=V1 ;NAME(127)=PRPS
NAME(128)=LTLS ;NAME(129)=ENTI
NAME(130)=CP ;NAME(131)=SHRY
NAME(132)=SHRX ;NAME(133)=CF
NAME(134)=NENU ;NAME(135)=DWDY
NAME(136)=DWDX ;NAME(137)=DVDZ
NAME(138)=DUDZ ;NAME(139)=DVDX
NAME(140)=DUDY ;NAME(141)=MACH
NAME(142)=WDIS ;NAME(143)=VOR1
NAME(144)=STRS ;NAME(145)=SKIN
NAME(146)=YPLS ;NAME(147)=ENUL
NAME(148)=DEN1 ;NAME(149)=EL1
NAME(150)=ENUT
* Y in SOLUTN argument list denotes:
* 1-stored 2-solved 3-whole-field
* 4-point-by-point 5-explicit 6-harmonic averaging
SOLUTN(P1,Y,Y,Y,N,N,Y)
SOLUTN(U1,Y,Y,Y,N,N,Y)
SOLUTN(V1,Y,Y,Y,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
SOLUTN(LTLS,Y,Y,Y,N,N,Y)
SOLUTN(ENTI,Y,Y,Y,N,N,Y)
SOLUTN(CP,Y,N,N,N,N,Y)
SOLUTN(SHRY,Y,N,N,N,N,Y)
SOLUTN(SHRX,Y,N,N,N,N,Y)
SOLUTN(CF,Y,N,N,N,N,Y)
SOLUTN(NENU,Y,N,N,N,N,Y)
SOLUTN(DWDY,Y,N,N,N,N,Y)
SOLUTN(DWDX,Y,N,N,N,N,Y)
SOLUTN(DVDZ,Y,N,N,N,N,Y)
SOLUTN(DUDZ,Y,N,N,N,N,Y)
SOLUTN(DVDX,Y,N,N,N,N,Y)
SOLUTN(DUDY,Y,N,N,N,N,Y)
SOLUTN(MACH,Y,N,N,N,N,Y)
SOLUTN(WDIS,Y,N,N,N,N,Y)
SOLUTN(VOR1,Y,N,N,N,N,Y)
SOLUTN(STRS,Y,N,N,N,N,Y)
SOLUTN(SKIN,Y,N,N,N,N,Y)
SOLUTN(YPLS,Y,N,N,N,N,Y)
SOLUTN(ENUL,Y,N,N,N,N,Y)
SOLUTN(DEN1,Y,N,N,N,N,Y)
SOLUTN(EL1,Y,N,N,N,N,Y)
SOLUTN(ENUT,Y,N,N,N,N,Y)
DEN1 = 148
VISL = 147
VIST = 150
LEN1 = 149
PRPS = 127
************************************************************
Group 8. Terms & Devices
* Y in TERMS argument list denotes:
* 1-built-in source 2-convection 3-diffusion 4-transient
* 5-first phase variable 6-interphase transport
TERMS(P1,Y,Y,Y,N,Y,Y)
TERMS(U1,Y,Y,Y,Y,Y,Y)
TERMS(V1,Y,Y,Y,Y,Y,Y)
TERMS(LTLS,N,N,Y,N,Y,Y)
TERMS(ENTI,N,Y,Y,Y,N,Y)
DIFCUT =0.5 ;ZDIFAC =1.
GALA = F ;ADDDIF = F
NEWENT = F
ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
************************************************************
Group 9. Properties used if PRPS is not
stored, and where PRPS = -1.0 if it is!
RHO1 =1.189 ;TMP1 =0. ;EL1 =0.
TSURR =0. ;TEMP0 =273.149994 ;PRESS0 =1.01325E+05
DVO1DT =3.41E-03 ;DRH1DP =0.
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
ENUL =1.544E-05 ;ENUT = GRND2
ENUTA =0. ;ENUTB =0. ;ENUTC =0.
IENUTA = 21
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRNDTL(LTLS)=1. ;PRNDTL(ENTI)=0.666667
PRT(U1)=1. ;PRT(V1)=1.
PRT(LTLS)=1. ;PRT(ENTI)=0.666667
CP1 =1005. ;CP2 =1.
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(P1)=0. ;FIINIT(U1)=1.0E-10
FIINIT(V1)=1.0E-10 ;FIINIT(PRPS)=-1.
FIINIT(LTLS)=1.0E-10 ;FIINIT(ENTI)=4.632E-05
FIINIT(CP)=1.0E-10 ;FIINIT(SHRY)=1.0E-10
FIINIT(SHRX)=1.0E-10 ;FIINIT(CF)=1.0E-10
FIINIT(NENU)=1.0E-10 ;FIINIT(DWDY)=1.0E-10
FIINIT(DWDX)=1.0E-10 ;FIINIT(DVDZ)=1.0E-10
FIINIT(DUDZ)=1.0E-10 ;FIINIT(DVDX)=1.0E-10
FIINIT(DUDY)=1.0E-10 ;FIINIT(MACH)=1.0E-10
FIINIT(WDIS)=0.1 ;FIINIT(VOR1)=1.0E-10
FIINIT(STRS)=1.0E-10 ;FIINIT(SKIN)=1.0E-10
FIINIT(YPLS)=1.0E-10 ;FIINIT(ENUL)=1.0E-10
FIINIT(DEN1)=1.0E-10 ;FIINIT(EL1)=1.0E-10
FIINIT(ENUT)=1.0E-10
PATCH(^OBA ,INIVAL, 10, 0, 0, 0, 0, 0, 1, 1)
INIT(^OBA ,PRPS,0. ,198. )
INIADD = F
FSWEEP = 1
NAMFI =CHAM
************************************************************
Group 12. Patchwise adjustment of terms
Patches for this group are printed with those
for Group 13.
Their names begin either with GP12 or &
************************************************************
Group 13. Boundary & Special Sources
PATCH(SASOPRO ,PHASEM, 1, 241, 1, 139, 1, 1, 1, 1)
COVAL(SASOPRO ,ENTI, FIXFLU , GRND4 )
PATCH(SASODIS ,PHASEM, 1, 241, 1, 139, 1, 1, 1, 1)
COVAL(SASODIS ,ENTI, GRND4 ,0. )
PATCH(SASODIF ,PHASEM, 1, 241, 1, 139, 1, 1, 1, 1)
COVAL(SASODIF ,ENTI, FIXFLU , GRND4 )
PATCH(^OB1 ,WEST , 1, 0, 0, 0, 0, 0, 1, 1)
COVAL(^OB1 ,P1 , FIXFLU ,21.9965 )
COVAL(^OB1 ,U1 ,0. ,18.5 )
COVAL(^OB1 ,V1 ,0. ,0. )
COVAL(^OB1 ,ENTI,0. ,4.632E-05 )
PATCH(^OB2 ,EAST , 2, 0, 0, 0, 0, 0, 1, 1)
COVAL(^OB2 ,P1 ,1000. ,0. )
COVAL(^OB2 ,U1 ,0. ,0. )
COVAL(^OB2 ,V1 ,0. ,0. )
COVAL(^OB2 ,ENTI,0. ,4.632E-05 )
PATCH(^OB3 ,SOUTH , 3, 0, 0, 0, 0, 0, 1, 1)
COVAL(^OB3 ,P1 ,1000. ,0. )
COVAL(^OB3 ,U1 ,0. ,18.5 )
COVAL(^OB3 ,V1 ,0. ,0. )
COVAL(^OB3 ,ENTI,0. ,4.632E-05 )
PATCH(^OB4 ,NORTH , 4, 0, 0, 0, 0, 0, 1, 1)
COVAL(^OB4 ,P1 ,1000. ,0. )
COVAL(^OB4 ,U1 ,0. ,18.5 )
COVAL(^OB4 ,V1 ,0. ,0. )
COVAL(^OB4 ,ENTI,0. ,4.632E-05 )
XCYCLE = F
EGWF = T
WALLCO = GRND2
SCALWF = T
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 3000 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-05
************************************************************
Group 16. Terminate Iterations
LITER(P1)=200 ;LITER(U1)=10
LITER(V1)=10 ;LITER(LTLS)=20
LITER(ENTI)=40
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03 ;ENDIT(LTLS)=1.0E-03
ENDIT(ENTI)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(U1,FALSDT,4.0E-03)
RELAX(V1,FALSDT,4.0E-03)
RELAX(PRPS,LINRLX,1.)
RELAX(LTLS,LINRLX,1.)
RELAX(ENTI,LINRLX,0.3)
RELAX(CP,LINRLX,1.)
RELAX(SHRY,LINRLX,1.)
RELAX(SHRX,LINRLX,1.)
RELAX(CF,LINRLX,1.)
RELAX(NENU,LINRLX,1.)
RELAX(DWDY,LINRLX,1.)
RELAX(DWDX,LINRLX,1.)
RELAX(DVDZ,LINRLX,1.)
RELAX(DUDZ,LINRLX,1.)
RELAX(DVDX,LINRLX,1.)
RELAX(DUDY,LINRLX,1.)
RELAX(MACH,LINRLX,1.)
RELAX(WDIS,LINRLX,1.)
RELAX(VOR1,LINRLX,1.)
RELAX(STRS,LINRLX,1.)
RELAX(SKIN,LINRLX,1.)
RELAX(YPLS,LINRLX,1.)
RELAX(ENUL,LINRLX,1.)
RELAX(DEN1,LINRLX,1.)
RELAX(EL1,LINRLX,1.)
RELAX(ENUT,LINRLX,1.)
OVRRLX =0.
EXPERT = F ;NNORSL = F
************************************************************
Group 18. Limits
VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
VARMAX(U1)=1.0E+06 ;VARMIN(U1)=-1.0E+06
VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
VARMAX(LTLS)=1.0E+10 ;VARMIN(LTLS)=-1.0E+10
VARMAX(ENTI)=1.0E+10 ;VARMIN(ENTI)=1.0E-10
VARMAX(CP)=1.0E+10 ;VARMIN(CP)=-1.0E+10
VARMAX(SHRY)=1.0E+10 ;VARMIN(SHRY)=-1.0E+10
VARMAX(SHRX)=1.0E+10 ;VARMIN(SHRX)=-1.0E+10
VARMAX(CF)=1.0E+10 ;VARMIN(CF)=-1.0E+10
VARMAX(NENU)=1.0E+10 ;VARMIN(NENU)=-1.0E+10
VARMAX(DWDY)=1.0E+10 ;VARMIN(DWDY)=-1.0E+10
VARMAX(DWDX)=1.0E+10 ;VARMIN(DWDX)=-1.0E+10
VARMAX(DVDZ)=1.0E+10 ;VARMIN(DVDZ)=-1.0E+10
VARMAX(DUDZ)=1.0E+10 ;VARMIN(DUDZ)=-1.0E+10
VARMAX(DVDX)=1.0E+10 ;VARMIN(DVDX)=-1.0E+10
VARMAX(DUDY)=1.0E+10 ;VARMIN(DUDY)=-1.0E+10
VARMAX(MACH)=1.0E+10 ;VARMIN(MACH)=-1.0E+10
VARMAX(WDIS)=1.0E+10 ;VARMIN(WDIS)=-1.0E+10
VARMAX(VOR1)=1.0E+10 ;VARMIN(VOR1)=-1.0E+10
VARMAX(STRS)=1.0E+10 ;VARMIN(STRS)=-1.0E+10
VARMAX(SKIN)=1.0E+10 ;VARMIN(SKIN)=-1.0E+10
VARMAX(YPLS)=1.0E+10 ;VARMIN(YPLS)=-1.0E+10
VARMAX(ENUL)=1.0E+10 ;VARMIN(ENUL)=-1.0E+10
VARMAX(DEN1)=1.0E+10 ;VARMIN(DEN1)=-1.0E+10
VARMAX(EL1)=1.0E+10 ;VARMIN(EL1)=-1.0E+10
VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
GENK = T
CALFOR = T
IENUTA = 21
ISG62 = 0
SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,0)
SPEDAT(SET,GXMONI,PLOTALL,L,T)
SPEDAT(SET,GXMONI,MINIRES,L,F)
SPEDAT(SET,STORED,NENU,C,=ENUT/ENUL!ZSLFIN)
SPEDAT(SET,MAKE,UINF,C,=0.)
SPEDAT(SET,STORED,UINF,C,=18.5!ZSLFIN)
SPEDAT(SET,STORED,CF,C,=2*STRS/(UINF^2)!SWPFIN)
SPEDAT(SET,STORED,CP,C,=(P1)/(0.5*DEN1*UINF^2)!SWPFIN)
SPEDAT(SET,DRAG,CDCALC,C,YES)
SPEDAT(SET,DRAG,REFDEN,R,1.189)
SPEDAT(SET,DRAG,REFVEL,R,18.5)
SPEDAT(SET,DRAG,REFARX,R,1.)
SPEDAT(SET,DRAG,REFARY,R,1.)
SPEDAT(SET,DRAG,REFARZ,R,0.)
SPEDAT(SET,DRAG,MOMCENX,R,0.)
SPEDAT(SET,DRAG,MOMCENY,R,0.)
SPEDAT(SET,DRAG,MOMCENZ,R,0.)
SPEDAT(SET,OBJNAM,^OB1,C,INL)
SPEDAT(SET,OBJTYP,^OB1,C,INLET)
SPEDAT(SET,OBJNAM,^OB2,C,OUT)
SPEDAT(SET,OBJTYP,^OB2,C,OUTLET)
SPEDAT(SET,ARATIO,^OB2,R,1.)
SPEDAT(SET,OBJNAM,^OB3,C,FAR_S)
SPEDAT(SET,OBJTYP,^OB3,C,OUTLET)
SPEDAT(SET,ARATIO,^OB3,R,1.)
SPEDAT(SET,OBJNAM,^OB4,C,FAR_N)
SPEDAT(SET,OBJTYP,^OB4,C,OUTLET)
SPEDAT(SET,ARATIO,^OB4,R,1.)
SPEDAT(SET,OBJNAM,!OB5,C,NULL0)
SPEDAT(SET,OBJTYP,!OB5,C,NULL)
SPEDAT(SET,OBJNAM,!OB6,C,NULL1)
SPEDAT(SET,OBJTYP,!OB6,C,NULL)
SPEDAT(SET,OBJNAM,!OB7,C,NULL2)
SPEDAT(SET,OBJTYP,!OB7,C,NULL)
SPEDAT(SET,OBJNAM,!OB8,C,NULL3)
SPEDAT(SET,OBJTYP,!OB8,C,NULL)
SPEDAT(SET,OBJNAM,!OB9,C,NULL4)
SPEDAT(SET,OBJTYP,!OB9,C,NULL)
SPEDAT(SET,OBJNAM,^OBA,C,AEROFOIL)
SPEDAT(SET,OBJTYP,^OBA,C,BLOCKAGE)
SPEDAT(SET,AEROFOIL,MATERIAL,R,198.)
SPEDAT(SET,FACETDAT,NUMOBJ,I,17)
SPEDAT(SET,MATERIAL,198,L,T)
************************************************************
Group 20. Preliminary Printout
DISTIL = T ;NULLPR = F
NDST = 0
DSTTOL =1.0E-02
EX(P1)=10.76 ;EX(U1)=17.08
EX(V1)=0.5833 ;EX(PRPS)=0.9377
EX(LTLS)=2.588 ;EX(ENTI)=1.154E-04
EX(CP)=0.0529 ;EX(SHRY)=1.016E-03
EX(SHRX)=8.957E-03 ;EX(CF)=5.48E-05
EX(NENU)=5.047 ;EX(DWDY)=9.377E-11
EX(DWDX)=9.377E-11 ;EX(DVDZ)=9.377E-11
EX(DUDZ)=9.377E-11 ;EX(DVDX)=3.734
EX(DUDY)=24.83 ;EX(MACH)=0.04959
EX(WDIS)=0.7992 ;EX(VOR1)=22.43
EX(STRS)=9.377E-03 ;EX(SKIN)=1.368E-03
EX(YPLS)=0.4643 ;EX(ENUL)=1.448E-05
EX(DEN1)=1.115 ;EX(EL1)=0.
EX(ENUT)=7.792E-05
************************************************************
Group 21. Print-out of Variables
INIFLD = F ;SUBWGR = F
* Y in OUTPUT argument list denotes:
* 1-field 2-correction-eq. monitor 3-selective dumping
* 4-whole-field residual 5-spot-value table 6-residual table
OUTPUT(P1,N,N,Y,Y,Y,Y)
OUTPUT(U1,N,N,Y,Y,Y,Y)
OUTPUT(V1,N,N,Y,Y,Y,Y)
OUTPUT(PRPS,N,N,Y,N,N,N)
OUTPUT(LTLS,N,N,Y,Y,Y,Y)
OUTPUT(ENTI,N,N,Y,Y,Y,Y)
OUTPUT(CP,N,N,Y,N,N,N)
OUTPUT(SHRY,N,N,Y,N,N,N)
OUTPUT(SHRX,N,N,Y,N,N,N)
OUTPUT(CF,N,N,Y,N,N,N)
OUTPUT(NENU,N,N,Y,N,N,N)
OUTPUT(DWDY,N,N,Y,N,N,N)
OUTPUT(DWDX,N,N,Y,N,N,N)
OUTPUT(DVDZ,N,N,Y,N,N,N)
OUTPUT(DUDZ,N,N,Y,N,N,N)
OUTPUT(DVDX,N,N,Y,N,N,N)
OUTPUT(DUDY,N,N,Y,N,N,N)
OUTPUT(MACH,N,N,Y,N,N,N)
OUTPUT(WDIS,N,N,Y,N,N,N)
OUTPUT(VOR1,N,N,Y,N,N,N)
OUTPUT(STRS,N,N,Y,N,N,N)
OUTPUT(SKIN,N,N,Y,N,N,N)
OUTPUT(YPLS,N,N,Y,N,N,N)
OUTPUT(ENUL,N,N,Y,N,N,N)
OUTPUT(DEN1,N,N,Y,N,N,N)
OUTPUT(EL1,N,N,Y,N,N,N)
OUTPUT(ENUT,N,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 77 ;IYMON = 54 ;IZMON = 1
NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
UWATCH = T ;USTEER = T
HIGHLO = F
************************************************************
Group 23.Field Print-Out & Plot Control
NPRINT = 100000 ;NUMCLS = 5
NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 10000
NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 10000
IPLTF = 1 ;IPLTL = -1 ;NPLT = -1
ISWPRF = 1 ;ISWPRL = 100000
ITABL = 3 ;IPROF = 1
ABSIZ =0.5 ;ORSIZ =0.4
NTZPRF = 1 ;NCOLPF = 50
ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
No PATCHes yet used for this Group
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP