$ $file prop3.dat $ $ The dmap propa.v2001 is not needed for this run. The features $ are included in SOL 145. $ ID PROP, PROP3 $ FILE BAH_NEW_2000 = TEST OF BALANCED MASS - 2000 rpm $ $ SAMPLE AERO PROBLEM WITH PROP TERMS - BAH WING/NACELLE WITH 7 FT PROP $ INCLUDING WASH TERMS 11/30/1988 - BAH_FWASH.DAT $ TIME 100 sol 145 CEND TITLE = PROP WHIRL SAMPLE - BAH WING/NACELLE WITH 7 FT 4-BLADE PROP3 SUBT = SAMPLE PROBLEM WITH WASH-2000RPM- HIGH SSOUND - BAH_NEW2000 LABEL = PK-FLUTTER SOLUTION SEALL = ALL $ SOL 75 HAS SUPERELEMENT CAPABILITY ECHO = BOTH $ ANNOTATED AND SORTED INPUT DATA SPC = 1 $ CONSTRAINT AT FUSELAGE/WING-E.A. INTERSECTION MPC = 99 $ CONSTRAINTS FOR NACELLE ROTATIONS METHOD = 10 $ MODIFIED GIVENS FOR VIBES SVEC = ALL $ PRINT VIBRATION MODES DISP = ALL $ PRINT FLUTTER MODES SDAMP = 2000 $ INCLUDE 1% STRUCTURAL DAMPING ON ALL MODES SUBCASE 10 FMETHOD = 5 $ PK-FLUTTER METHOD - V = 6000 K2PP=AEROS101 B2PP=AEROB101 SUBCASE 14 FMETHOD = 10 $ PK-FLUTTER METHOD - V = 7200 K2PP=AEROS102 B2PP=AEROB102 SUBCASE 20 FMETHOD = 20 $ PK-FLUTTER METHOD - V = 8400 K2PP=AEROS103 B2PP=AEROB103 SUBCASE 30 FMETHOD = 30 $ PK-FLUTTER METHOD - V = 9600 K2PP=AEROS104 B2PP=AEROB104 SUBCASE 40 FMETHOD = 40 $ PK-FLUTTER METHOD - V = 10800 K2PP=AEROS105 B2PP=AEROB105 SUBCASE 50 FMETHOD = 50 $ PK-FLUTTER METHOD - V = 12000 K2PP=AEROS106 B2PP=AEROB106 SUBCASE 60 FMETHOD = 60 $ PK-FLUTTER METHOD - V = 13200 K2PP=AEROS107 B2PP=AEROB107 SUBCASE 70 FMETHOD = 70 $ PK-FLUTTER METHOD - V = 14400 K2PP=AEROS108 B2PP=AEROB108 SUBCASE 80 FMETHOD = 80 $ PK-FLUTTER METHOd - V = 15600 K2PP=AEROS109 B2PP=AEROB109 SUBCASE 82 FMETHOD = 82 $ PK-FLUTTER METHOd - V = 15900 K2PP=AEROS110 B2PP=AEROB110 SUBCASE 84 FMETHOD = 84 $ PK-FLUTTER METHOd - V = 16200 K2PP=AEROS111 B2PP=AEROB111 SUBCASE 90 FMETHOD = 90 $ PK-FLUTTER METHOD - V = 16800 K2PP=AEROS112 B2PP=AEROB112 SUBCASE 100 FMETHOD = 100 $ PK-FLUTTER METHOD - V = 18000 K2PP=AEROS113 B2PP=AEROB113 SUBCASE 110 FMETHOD = 110 $ PK-FLUTTER METHOD - V = 19200 K2PP=AEROS114 B2PP=AEROB114 SUBCASE 120 FMETHOD = 120 $ PK-FLUTTER METHOD - V = 20400 K2PP=AEROS115 B2PP=AEROB115 SUBCASE 130 FMETHOD = 130 $ PK-FLUTTER METHOD - V = 21600 K2PP=AEROS116 B2PP=AEROB116 SUBCASE 140 FMETHOD = 140 $ PK-FLUTTER METHOD - V = 22800 K2PP=AEROS117 B2PP=AEROB117 SUBCASE 150 FMETHOD = 150 $ PK-FLUTTER METHOD - V = 24000 K2PP=AEROS118 B2PP=AEROB118 BEGIN BULK $ $ PROP HUB IS GRID 99 - ATTACHED TO SPOINTS VIA MPCS FOR FREQUENCIES $ GRID 99 137.48 186.0 0.0 15 14 $ RELATIVE PITCH ANGLE OF NACELLE SPOINT 100 $ RELATIVE YAW ANGLE OF NACELLE SPOINT 102 $ MPCS FOR NACELLE SPRINGS AND HUB DOFS $ SID G C A G C A ETC MPC 99 100 119.63 3 3 -2.34039 +MPC100 +MPC100 4 3 1.34039 99 3 1.0 MPC 99 99 5 89.25 3 3 1.0 +MPC101 +MPC101 4 3 -1.0 100 -89.25 MPC 99 102 119.63 99 2 -1.0 MPC 99 99 6 1.0 102 -1.0 $ $2345678123456781234567812345678123456781234567812345678123456781234567812345678 $ CONCENTRATED MASS FOR PROP $ EID G CID M X1 X2 X3 CONM2 99 99 400.0 +PROP $ I11 I21 I22 I31 I32 I33 +PROP 864000. 432000. 432000. $ $ CELAS4 SPRINGS FOR NACELLE ATTACHMENT $ $ PITCH SPRING $ EID K S1 S2 ETC CELAS4 1 19.2+6 100 $ YAW SPRING CELAS4 2 24.0+6 102 $ $BAH WING DATA FROM HA75B.DAT AERO 1 131.232 1.1468-71 $ INB0ARD WING AERO $ EID PID CP NSPAN NCHORD LSPAN LCHORD IGID +CONT CAERO1 1001 1001 0 4 77 1 +CA1 $ X1 Y1 Z1 X12 X4 Y4 Z4 X14 +CA1 78.75 0.0 0.0 225.0 35.0 500.0 0.0 100.0 AEFACT 77 .0 .09 .213 .336 $ OUTBOARD WING AERO CAERO1 1013 1001 0 4 78 1 +CA13 +CA13 78.75 0.0 0.0 225.0 35.0 500.0 0.0 100.0 AEFACT 78 .408 .556 .704 .852 1.0 $ PID B1 B2 B3 ETC PAERO1 1001 2001 $ INBOARD WING SPLINE SPLINE2 101 1001 1005 1012 14 0.0 1.0 0 +SP101 +SP101 -1.0 -1.0 SET1 14 1 THRU 11 $ OUTBOARD WING SPLINE SPLINE2 113 1013 1013 1028 15 0.0 1.0 0 +SP113 +SP113 -1.0 -1.0 SET1 15 1 THRU 11 $ENGINE NACELLE AERO VIA CAERO2 & PAERO2 AT W.S. 186.0 $ EID PID CP NSB NINT LSB LINT IGID +CONT CAERO2 2001 2001 0 2001 2001 1 +CA2 $ X1 Y1 Z1 X12 +CA2 162.48 186.0 0.0 278.5 AEFACT 2001 0.0 0.180 0.359 0.593 0.680 0.840 1.0 $ PID ORIENT WIDTH AR LRSB LRIB LTH1 LTH2 +CONT PAERO2 2001 Z 18.0 1.0 2010 2018 +PA2 $ THI1 THN1 THI2 THN2 +PA2 1 6 AEFACT 2010 0.0 13.5 18.0 18.0 18.0 18.0 18.0 AEFACT 2018 90.0 270.0 $ NACELLE SPLINE SPLINE2 201 2001 2001 2006 16 0.0 1.0 0 +SP201 +SP201 -1.0 SET1 16 3 4 99 $ $ if it is desired not to include propeller slipstream effects, remove $ the DMIG entries for WKK $ (these effects are not included in the reference paper) $ $CORRECTION FACTORS FOR PROP SLIPSTREAM; N.B., THERE ARE 68 CORRECTION $FACTORS, ONE FOR LIFT & ONE FOR MOMENT ON EACH ELEMENT -- THERE ARE 34 AERO $ELEMENTS: 28 WING BOXES + 6 SLENDER BODY ELEMENTS. DMI WKK 0 3 1 68 1 $1ST 2 ROWS OF BOXES ON WING HAVE WKK=1.0, 3RD ROW OF BOXES ON WING INBOARD $OF NACELLE HAS WKK=1.0181, 4TH ROW OF BOXES ON WING OUTBOARD OF NACELLE HAS $WKK=1.0150, 5TH THRU 7TH ROWS OF WING BOXES HAVE WKK=1.0, 2 NACELLE SLENDER $BODY ELEMENTS FORWARD OF WING HAVE WKK=1.0232, AND 4 NACELLE SLENDER BODY $ELEMENTS ON WING HAVE WKK=1.0467. DMI WKK 1 1 1.0 THRU 16 17 1.0181 +DMI1 +DMI1 THRU 24 25 1.0150 THRU 32 33 1.0 +DMI2 +DMI2 THRU 56 57 1.0232 THRU 60 61 1.0467 +DMI3 +DMI3 THRU 68 CMASS2 121 5248.7 1 3 CMASS2 122 134.9 1 3 2 3 CMASS2 123 790.3 2 3 CMASS2 341 8791.3 3 3 CMASS2 342 9696.1 3 3 4 3 CMASS2 343 1008.7 4 3 CMASS2 561 3253.6 5 3 CMASS2 562 -139.7 5 3 6 3 CMASS2 563 946.3 6 3 CMASS2 781 2617.8 7 3 CMASS2 782 21. 7 3 8 3 CMASS2 783 782.3 8 3 CMASS2 9101 494.8 9 3 CMASS2 9102 -7.3 9 3 10 3 CMASS2 9103 185.2 10 3 CONM1 1 11 +51 +51 17400. 4.37+7 +52 +52 4.35+09 $ $ coordinate system for prop point $ CORD2R 15 0. 0. 0. 0. 0. 1. +cr15 +cr15 1. 0. 0. CORD2R 1 0. 0. 0. 0. 0. -1. +C1 +C1 -1. 0. 0. EIGR 10 MGIV 12 +EIGR +EIGR MAX FLFACT 1 1. DENSITY FLFACT 2 .0 MACH NO FLFACT 3 6000. VELOCITY FLFACT 4 7200. VELOCITY FLFACT 5 8400. VELOCITY FLFACT 6 9600. VELOCITY FLFACT 7 10800. VELOCITY FLFACT 8 12000. VELOCITY FLFACT 9 13200. VELOCITY FLFACT 10 14400. VELOCITY FLFACT 11 15600. VELOCITY FLFACT 12 16800. VELOCITY FLFACT 13 18000. VELOCITY FLFACT 14 19200. VELOCITY FLFACT 15 20400. VELOCITY FLFACT 16 21600. VELOCITY FLFACT 17 22800. VELOCITY FLFACT 18 24000. VELOCITY FLFACT 19 15900. VELOCITY FLFACT 20 16200. VELOCITY FLUTTER 5 PK 1 2 3 L 5 FLUTTER 10 PK 1 2 4 L 5 FLUTTER 20 PK 1 2 5 L 5 FLUTTER 30 PK 1 2 6 L 5 FLUTTER 40 PK 1 2 7 L 5 FLUTTER 50 PK 1 2 8 L 5 FLUTTER 60 PK 1 2 9 L 5 FLUTTER 70 PK 1 2 10 L 5 FLUTTER 80 PK 1 2 11 L 5 FLUTTER 82 PK 1 2 19 L 5 FLUTTER 84 PK 1 2 20 L 5 FLUTTER 90 PK 1 2 12 L 5 FLUTTER 100 PK 1 2 13 L 5 FLUTTER 110 PK 1 2 14 L 5 FLUTTER 120 PK 1 2 15 L 5 FLUTTER 130 PK 1 2 16 L 5 FLUTTER 140 PK 1 2 17 L 5 FLUTTER 150 PK 1 2 18 L 5 GENEL 432 1 3 2 3 3 3 +01 +01 4 3 5 3 6 3 7 3 +02 +02 8 3 9 3 10 3 +03 +03 UD 11 3 11 5 +04 +04 Z 8.7172-61.3361-61.2778-56.2720-61.6251-51.0492-52.0478-5+05 +05 1.5630-52.4285-52.0403-53.0861-56.2720-63.2297-51.0492-53.3529-5+06 +06 1.5630-53.5021-52.0257-53.5785-52.7732-51.5726-54.8255-53.7628-5+07 +07 7.3284-56.4338-59.5810-58.8378-56.3749-53.7628-58.0136-56.4338-5+08 +08 1.0012-48.8378-51.1811-41.2758-41.1344-41.9350-41.8160-42.5283-4+09 +09 2.4294-41.6999-41.8160-42.2920-42.4294-42.8249-43.6862-43.5052-4+10 +10 5.2675-45.1171-44.2292-45.1171-45.7187-48.4840-48.2340-49.2340-4+11 +11 S 1.0 -20.25 1.0 81.0 1.0 -17.85 1.0 +12 +12 71.4 1.0 -15.8 1.0 63.2 1.0 -13.3 1.0 +13 +13 53.2 1.0 -11.05 1.0 44.2 GRID 1 20.25 90. 12456 GRID 2 -81. 90. 12456 GRID 3 17.85 186. 12456 GRID 4 -71.4 186. 12456 GRID 5 15.8 268. 12456 GRID 6 -63.2 268. 12456 GRID 7 13.3 368. 12456 GRID 8 -53.2 368. 12456 GRID 9 11.05 458. 12456 GRID 10 -44.2 458. 12456 GRID 11 0.0 0. 1246 MKAERO1 0. +MK +MK 0.001 0.05 0.10 0.20 0.50 1.0 PARAM GRDPNT 11 PARAM KDAMP -1 PARAM W4 57.554 PARAM LMODES 12 PARAM VREF 12.0 PARAM WTMASS .0025901 SPC1 1 35 11 $ $ ADD TABDMP1 FOR STRUCTURAL DAMPING $ TABDMP1 2000 +T2000 +T2000 0.0 0.00 10.0 0.00 ENDT $ $ THE FOLLOWING CARDS ARE THE PROPELLER DMIG MATRICES $ (normally an include statement would be used) $INCLUDE 'aerodmig.dat' $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS101 AND AEROB101) ARE BASED ON $ VELOCITY = 5.000000E+02(ft/sec) $ MACH NO = 5.000000E-05 $ DENSITY = 1.146800E-07 DMIG AEROS101 0 1 1 DMIG *AEROS101 99 3 *S100000 *S100000 1 3-1.168915367E+01 *S100001 *S100001 2 3 1.168920898E+01 *S100002 *S100002 3 3-9.017248154E+00 *S100003 *S100003 4 3 9.216135025E+00 *S100004 *S100004 5 3-1.034624672E+01 *S100005 *S100005 6 3 1.034629250E+01 *S100006 *S100006 7 3-7.776564598E+00 *S100007 *S100007 8 3 7.776603222E+00 *S100008 *S100008 9 3-5.130343437E+00 *S100009 *S100009 10 3 5.130365372E+00 *S100010 *S100010 99 3-1.988494247E-01 *S100011 *S100011 99 5 0.000000000E+00 *S100012 *S100012 99 2 0.000000000E+00 *S100013 *S100013 99 6 0.000000000E+00 *S100014 DMIG *AEROS101 99 5 *S100015 *S100015 1 3 7.855181122E+01 *S100016 *S100016 2 3-7.855218506E+01 *S100017 *S100017 3 3 6.059645081E+01 *S100018 *S100018 4 3-6.193297958E+01 *S100019 *S100019 5 3 6.952739716E+01 *S100020 *S100020 6 3-6.952770996E+01 *S100021 *S100021 7 3 5.225897980E+01 *S100022 *S100022 8 3-5.225923920E+01 *S100023 *S100023 9 3 3.447621536E+01 *S100024 *S100024 10 3-3.447636032E+01 *S100025 *S100025 99 3 4.624994629E+03 *S100026 *S100026 99 5-3.107125977E+04 *S100027 *S100027 99 2-1.216591064E+03 *S100028 *S100028 99 6 1.198435625E+05 *S100029 DMIG *AEROS101 99 2 *S100030 *S100030 1 3 3.075685740E+00 *S100031 *S100031 2 3-3.075700521E+00 *S100032 *S100032 3 3 2.372645855E+00 *S100033 *S100033 4 3-2.424977541E+00 *S100034 *S100034 5 3 2.722336054E+00 *S100035 *S100035 6 3-2.722348213E+00 *S100036 *S100036 7 3 2.046193361E+00 *S100037 *S100037 8 3-2.046203613E+00 *S100038 *S100038 9 3 1.349911690E+00 *S100039 *S100039 10 3-1.349917293E+00 *S100040 *S100040 99 3 5.232186988E-02 *S100041 *S100041 99 5 0.000000000E+00 *S100042 *S100042 99 2 0.000000000E+00 *S100043 *S100043 99 6 0.000000000E+00 *S100044 DMIG *AEROS101 99 6 *S100045 *S100045 1 3-3.029786682E+02 *S100046 *S100046 2 3 3.029801025E+02 *S100047 *S100047 3 3-2.337238464E+02 *S100048 *S100048 4 3 2.388789215E+02 *S100049 *S100049 5 3-2.681709900E+02 *S100050 *S100050 6 3 2.681722107E+02 *S100051 *S100051 7 3-2.015657654E+02 *S100052 *S100052 8 3 2.015667725E+02 *S100053 *S100053 9 3-1.329766693E+02 *S100054 *S100054 10 3 1.329772186E+02 *S100055 *S100055 99 3-1.221745117E+03 *S100056 *S100056 99 5-1.198435625E+05 *S100057 *S100057 99 2-4.623658203E+03 *S100058 *S100058 99 6-3.107125977E+04 *S100059 DMIG AEROB101 0 1 1 DMIG *AEROB101 99 3 *D100064 *D100064 99 3 7.706096768E-01 *D100065 *D100065 99 5-5.178543568E+00 *D100066 *D100066 99 2-2.027651668E-01 *D100067 *D100067 99 6 1.997392654E+01 *D100068 DMIG *AEROB101 99 5 *D100069 *D100069 99 3 0.000000000E+00 *D100070 *D100070 99 5 7.521439209E+02 *D100071 *D100071 99 2 1.997392845E+01 *D100072 *D100072 99 6-5.249324375E+05 *D100073 DMIG *AEROB101 99 2 *D100074 *D100074 99 3 2.027651668E-01 *D100075 *D100075 99 5 1.997392654E+01 *D100076 *D100076 99 2 7.706096768E-01 *D100077 *D100077 99 6 5.178543568E+00 *D100078 DMIG *AEROB101 99 6 *D100079 *D100079 99 3 1.997392845E+01 *D100080 *D100080 99 5 5.249324375E+05 *D100081 *D100081 99 2 0.000000000E+00 *D100082 *D100082 99 6 7.521439209E+02 *D100083 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS102 AND AEROB102) ARE BASED ON $ VELOCITY = 6.000000E+02(ft/sec) $ MACH NO = 6.000000E-05 $ DENSITY = 1.146800E-07 DMIG AEROS102 0 1 1 DMIG *AEROS102 99 3 *S100084 *S100084 1 3-1.849901009E+01 *S100085 *S100085 2 3 1.849909782E+01 *S100086 *S100086 3 3-1.427050877E+01 *S100087 *S100087 4 3 1.458526230E+01 *S100088 *S100088 5 3-1.637375259E+01 *S100089 *S100089 6 3 1.637382698E+01 *S100090 *S100090 7 3-1.230702877E+01 *S100091 *S100091 8 3 1.230708981E+01 *S100092 *S100092 9 3-8.119174004E+00 *S100093 *S100093 10 3 8.119208336E+00 *S100094 *S100094 99 3-3.146949410E-01 *S100095 *S100095 99 5 0.000000000E+00 *S100096 *S100096 99 2 0.000000000E+00 *S100097 *S100097 99 6 0.000000000E+00 *S100098 DMIG *AEROS102 99 5 *S100099 *S100099 1 3 1.034484024E+02 *S100100 *S100100 2 3-1.034488983E+02 *S100101 *S100101 3 3 7.980218506E+01 *S100102 *S100102 4 3-8.156232452E+01 *S100103 *S100103 5 3 9.156375122E+01 *S100104 *S100104 6 3-9.156415558E+01 *S100105 *S100105 7 3 6.882219696E+01 *S100106 *S100106 8 3-6.882254028E+01 *S100107 *S100107 9 3 4.540327835E+01 *S100108 *S100108 10 3-4.540346909E+01 *S100109 *S100109 99 3 7.319064453E+03 *S100110 *S100110 99 5-4.091913672E+04 *S100111 *S100111 99 2-1.894488159E+03 *S100112 *S100112 99 6 1.606205625E+05 *S100113 DMIG *AEROS102 99 2 *S100114 *S100114 1 3 4.789489746E+00 *S100115 *S100115 2 3-4.789512634E+00 *S100116 *S100116 3 3 3.694708824E+00 *S100117 *S100117 4 3-3.776200294E+00 *S100118 *S100118 5 3 4.239249706E+00 *S100119 *S100119 6 3-4.239268780E+00 *S100120 *S100120 7 3 3.186353445E+00 *S100121 *S100121 8 3-3.186369419E+00 *S100122 *S100122 9 3 2.102096319E+00 *S100123 *S100123 10 3-2.102105141E+00 *S100124 *S100124 99 3 8.147615194E-02 *S100125 *S100125 99 5 0.000000000E+00 *S100126 *S100126 99 2 0.000000000E+00 *S100127 *S100127 99 6 0.000000000E+00 *S100128 DMIG *AEROS102 99 6 *S100129 *S100129 1 3-4.060677185E+02 *S100130 *S100130 2 3 4.060696716E+02 *S100131 *S100131 3 3-3.132488403E+02 *S100132 *S100132 4 3 3.201579285E+02 *S100133 *S100133 5 3-3.594166870E+02 *S100134 *S100134 6 3 3.594183044E+02 *S100135 *S100135 7 3-2.701488953E+02 *S100136 *S100136 8 3 2.701502380E+02 *S100137 *S100137 9 3-1.782222290E+02 *S100138 *S100138 10 3 1.782229767E+02 *S100139 *S100139 99 3-1.901395996E+03 *S100140 *S100140 99 5-1.606205625E+05 *S100141 *S100141 99 2-7.317304688E+03 *S100142 *S100142 99 6-4.091913672E+04 *S100143 DMIG AEROB102 0 1 1 DMIG *AEROB102 99 3 *D100148 *D100148 99 3 1.016292334E+00 *D100149 *D100149 99 5-5.683213711E+00 *D100150 *D100150 99 2-2.631233633E-01 *D100151 *D100151 99 6 2.230841255E+01 *D100152 DMIG *AEROB102 99 5 *D100153 *D100153 99 3 0.000000000E+00 *D100154 *D100154 99 5 7.049004517E+02 *D100155 *D100155 99 2 2.230841255E+01 *D100156 *D100156 99 6-5.249324375E+05 *D100157 DMIG *AEROB102 99 2 *D100158 *D100158 99 3 2.631233633E-01 *D100159 *D100159 99 5 2.230841255E+01 *D100160 *D100160 99 2 1.016292334E+00 *D100161 *D100161 99 6 5.683213711E+00 *D100162 DMIG *AEROB102 99 6 *D100163 *D100163 99 3 2.230841255E+01 *D100164 *D100164 99 5 5.249324375E+05 *D100165 *D100165 99 2 0.000000000E+00 *D100166 *D100166 99 6 7.049004517E+02 *D100167 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS103 AND AEROB103) ARE BASED ON $ VELOCITY = 7.000000E+02(ft/sec) $ MACH NO = 7.000000E-05 $ DENSITY = 1.146800E-07 DMIG AEROS103 0 1 1 DMIG *AEROS103 99 3 *S100168 *S100168 1 3-2.705398560E+01 *S100169 *S100169 2 3 2.705411530E+01 *S100170 *S100170 3 3-2.086998940E+01 *S100171 *S100171 4 3 2.133030319E+01 *S100172 *S100172 5 3-2.394589233E+01 *S100173 *S100173 6 3 2.394599915E+01 *S100174 *S100174 7 3-1.799848557E+01 *S100175 *S100175 8 3 1.799857521E+01 *S100176 *S100176 9 3-1.187393475E+01 *S100177 *S100177 10 3 1.187398434E+01 *S100178 *S100178 99 3-4.602274895E-01 *S100179 *S100179 99 5 0.000000000E+00 *S100180 *S100180 99 2 0.000000000E+00 *S100181 *S100181 99 6 0.000000000E+00 *S100182 DMIG *AEROS103 99 5 *S100183 *S100183 1 3 1.285243073E+02 *S100184 *S100184 2 3-1.285249176E+02 *S100185 *S100185 3 3 9.914624023E+01 *S100186 *S100186 4 3-1.013330307E+02 *S100187 *S100187 5 3 1.137588043E+02 *S100188 *S100188 6 3-1.137593155E+02 *S100189 *S100189 7 3 8.550469971E+01 *S100190 *S100190 8 3-8.550512695E+01 *S100191 *S100191 9 3 5.640903473E+01 *S100192 *S100192 10 3-5.640927124E+01 *S100193 *S100193 99 3 1.070342188E+04 *S100194 *S100194 99 5-5.083793750E+04 *S100195 *S100195 99 2-2.713155029E+03 *S100196 *S100196 99 6 2.037830000E+05 *S100197 DMIG *AEROS103 99 2 *S100198 *S100198 1 3 6.859176159E+00 *S100199 *S100199 2 3-6.859209061E+00 *S100200 *S100200 3 3 5.291306496E+00 *S100201 *S100201 4 3-5.408012867E+00 *S100202 *S100202 5 3 6.071160316E+00 *S100203 *S100203 6 3-6.071187496E+00 *S100204 *S100204 7 3 4.563275337E+00 *S100205 *S100205 8 3-4.563298225E+00 *S100206 *S100206 9 3 3.010477304E+00 *S100207 *S100207 10 3-3.010489941E+00 *S100208 *S100208 99 3 1.166845188E-01 *S100209 *S100209 99 5 0.000000000E+00 *S100210 *S100210 99 2 0.000000000E+00 *S100211 *S100211 99 6 0.000000000E+00 *S100212 DMIG *AEROS103 99 6 *S100213 *S100213 1 3-5.151874390E+02 *S100214 *S100214 2 3 5.151899414E+02 *S100215 *S100215 3 3-3.974259949E+02 *S100216 *S100216 4 3 4.061917114E+02 *S100217 *S100217 5 3-4.560002136E+02 *S100218 *S100218 6 3 4.560022583E+02 *S100219 *S100219 7 3-3.427441101E+02 *S100220 *S100220 8 3 3.427458191E+02 *S100221 *S100221 9 3-2.261146393E+02 *S100222 *S100222 10 3 2.261155853E+02 *S100223 *S100223 99 3-2.721919189E+03 *S100224 *S100224 99 5-2.037830000E+05 *S100225 *S100225 99 2-1.070123535E+04 *S100226 *S100226 99 6-5.083793750E+04 *S100227 DMIG AEROB103 0 1 1 DMIG *AEROB103 99 3 *D100232 *D100232 99 3 1.273956656E+00 *D100233 *D100233 99 5-6.052135944E+00 *D100234 *D100234 99 2-3.229946494E-01 *D100235 *D100235 99 6 2.425988388E+01 *D100236 DMIG *AEROB103 99 5 *D100237 *D100237 99 3 0.000000000E+00 *D100238 *D100238 99 5 6.605399780E+02 *D100239 *D100239 99 2 2.425988388E+01 *D100240 *D100240 99 6-5.249324375E+05 *D100241 DMIG *AEROB103 99 2 *D100242 *D100242 99 3 3.229946494E-01 *D100243 *D100243 99 5 2.425988388E+01 *D100244 *D100244 99 2 1.273956656E+00 *D100245 *D100245 99 6 6.052135944E+00 *D100246 DMIG *AEROB103 99 6 *D100247 *D100247 99 3 2.425988388E+01 *D100248 *D100248 99 5 5.249324375E+05 *D100249 *D100249 99 2 0.000000000E+00 *D100250 *D100250 99 6 6.605399780E+02 *D100251 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS104 AND AEROB104) ARE BASED ON $ VELOCITY = 8.000000E+02(ft/sec) $ MACH NO = 8.000000E-05 $ DENSITY = 1.146800E-07 DMIG AEROS104 0 1 1 DMIG *AEROS104 99 3 *S100252 *S100252 1 3-3.738462448E+01 *S100253 *S100253 2 3 3.738480377E+01 *S100254 *S100254 3 3-2.883925438E+01 *S100255 *S100255 4 3 2.947533989E+01 *S100256 *S100256 5 3-3.308969879E+01 *S100257 *S100257 6 3 3.308984756E+01 *S100258 *S100258 7 3-2.487125969E+01 *S100259 *S100259 8 3 2.487138367E+01 *S100260 *S100260 9 3-1.640802956E+01 *S100261 *S100261 10 3 1.640809822E+01 *S100262 *S100262 99 3-6.359666586E-01 *S100263 *S100263 99 5 0.000000000E+00 *S100264 *S100264 99 2 0.000000000E+00 *S100265 *S100265 99 6 0.000000000E+00 *S100266 DMIG *AEROS104 99 5 *S100267 *S100267 1 3 1.531983337E+02 *S100268 *S100268 2 3-1.531990662E+02 *S100269 *S100269 3 3 1.181802902E+02 *S100270 *S100270 4 3-1.207869034E+02 *S100271 *S100271 5 3 1.355981750E+02 *S100272 *S100272 6 3-1.355987701E+02 *S100273 *S100273 7 3 1.019198532E+02 *S100274 *S100274 8 3-1.019203644E+02 *S100275 *S100275 9 3 6.723841095E+01 *S100276 *S100276 10 3-6.723869324E+01 *S100277 *S100277 99 3 1.479013867E+04 *S100278 *S100278 99 5-6.059778125E+04 *S100279 *S100279 99 2-3.659963135E+03 *S100280 *S100280 99 6 2.486597500E+05 *S100281 DMIG *AEROS104 99 2 *S100282 *S100282 1 3 9.252818108E+00 *S100283 *S100283 2 3-9.252862930E+00 *S100284 *S100284 3 3 7.137810707E+00 *S100285 *S100285 4 3-7.295244217E+00 *S100286 *S100286 5 3 8.189809799E+00 *S100287 *S100287 6 3-8.189846039E+00 *S100288 *S100288 7 3 6.155718803E+00 *S100289 *S100289 8 3-6.155749321E+00 *S100290 *S100290 9 3 4.061041832E+00 *S100291 *S100291 10 3-4.061058521E+00 *S100292 *S100292 99 3 1.574038416E-01 *S100293 *S100293 99 5 0.000000000E+00 *S100294 *S100294 99 2 0.000000000E+00 *S100295 *S100295 99 6 0.000000000E+00 *S100296 DMIG *AEROS104 99 6 *S100297 *S100297 1 3-6.286411743E+02 *S100298 *S100298 2 3 6.286441650E+02 *S100299 *S100299 3 3-4.849464722E+02 *S100300 *S100300 4 3 4.956425781E+02 *S100301 *S100301 5 3-5.564197998E+02 *S100302 *S100302 6 3 5.564223022E+02 *S100303 *S100303 7 3-4.182226563E+02 *S100304 *S100304 8 3 4.182247314E+02 *S100305 *S100305 9 3-2.759092407E+02 *S100306 *S100306 10 3 2.759104004E+02 *S100307 *S100307 99 3-3.670657227E+03 *S100308 *S100308 99 5-2.486597500E+05 *S100309 *S100309 99 2-1.478753223E+04 *S100310 *S100310 99 6-6.059778125E+04 *S100311 DMIG AEROB104 0 1 1 DMIG *AEROB104 99 3 *D100316 *D100316 99 3 1.540367842E+00 *D100317 *D100317 99 5-6.312268257E+00 *D100318 *D100318 99 2-3.812461197E-01 *D100319 *D100319 99 6 2.590205574E+01 *D100320 DMIG *AEROB104 99 5 *D100321 *D100321 99 3 0.000000000E+00 *D100322 *D100322 99 5 6.196284790E+02 *D100323 *D100323 99 2 2.590205383E+01 *D100324 *D100324 99 6-5.249324375E+05 *D100325 DMIG *AEROB104 99 2 *D100326 *D100326 99 3 3.812461197E-01 *D100327 *D100327 99 5 2.590205574E+01 *D100328 *D100328 99 2 1.540367842E+00 *D100329 *D100329 99 6 6.312268257E+00 *D100330 DMIG *AEROB104 99 6 *D100331 *D100331 99 3 2.590205383E+01 *D100332 *D100332 99 5 5.249324375E+05 *D100333 *D100333 99 2 0.000000000E+00 *D100334 *D100334 99 6 6.196284790E+02 *D100335 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS105 AND AEROB105) ARE BASED ON $ VELOCITY = 9.000000E+02(ft/sec) $ MACH NO = 9.000000E-05 $ DENSITY = 1.146800E-07 DMIG AEROS105 0 1 1 DMIG *AEROS105 99 3 *S100336 *S100336 1 3-4.950907898E+01 *S100337 *S100337 2 3 4.950931549E+01 *S100338 *S100338 3 3-3.819229889E+01 *S100339 *S100339 4 3 3.903467941E+01 *S100340 *S100340 5 3-4.382123184E+01 *S100341 *S100341 6 3 4.382143021E+01 *S100342 *S100342 7 3-3.293741989E+01 *S100343 *S100343 8 3 3.293758392E+01 *S100344 *S100344 9 3-2.172942543E+01 *S100345 *S100345 10 3 2.172951508E+01 *S100346 *S100346 99 3-8.422211409E-01 *S100347 *S100347 99 5 0.000000000E+00 *S100348 *S100348 99 2 0.000000000E+00 *S100349 *S100349 99 6 0.000000000E+00 *S100350 DMIG *AEROS105 99 5 *S100351 *S100351 1 3 1.771164703E+02 *S100352 *S100352 2 3-1.771173096E+02 *S100353 *S100353 3 3 1.366312103E+02 *S100354 *S100354 4 3-1.396447906E+02 *S100355 *S100355 5 3 1.567684631E+02 *S100356 *S100356 6 3-1.567691650E+02 *S100357 *S100357 7 3 1.178321152E+02 *S100358 *S100358 8 3-1.178327026E+02 *S100359 *S100359 9 3 7.773603058E+01 *S100360 *S100360 10 3-7.773635101E+01 *S100361 *S100361 99 3 1.958638672E+04 *S100362 *S100362 99 5-7.005862500E+04 *S100363 *S100363 99 2-4.722268066E+03 *S100364 *S100364 99 6 2.947850313E+05 *S100365 DMIG *AEROS105 99 2 *S100366 *S100366 1 3 1.193845081E+01 *S100367 *S100367 2 3-1.193850803E+01 *S100368 *S100368 3 3 9.209561348E+00 *S100369 *S100369 4 3-9.412690163E+00 *S100370 *S100370 5 3 1.056690311E+01 *S100371 *S100371 6 3-1.056695080E+01 *S100372 *S100372 7 3 7.942417145E+00 *S100373 *S100373 8 3-7.942456722E+00 *S100374 *S100374 9 3 5.239759922E+00 *S100375 *S100375 10 3-5.239781857E+00 *S100376 *S100376 99 3 2.030903399E-01 *S100377 *S100377 99 5 0.000000000E+00 *S100378 *S100378 99 2 0.000000000E+00 *S100379 *S100379 99 6 0.000000000E+00 *S100380 DMIG *AEROS105 99 6 *S100381 *S100381 1 3-7.452513428E+02 *S100382 *S100382 2 3 7.452548828E+02 *S100383 *S100383 3 3-5.749019165E+02 *S100384 *S100384 4 3 5.875820923E+02 *S100385 *S100385 5 3-6.596332397E+02 *S100386 *S100386 6 3 6.596361694E+02 *S100387 *S100387 7 3-4.958011169E+02 *S100388 *S100388 8 3 4.958035889E+02 *S100389 *S100389 9 3-3.270891724E+02 *S100390 *S100390 10 3 3.270905457E+02 *S100391 *S100391 99 3-4.734945801E+03 *S100392 *S100392 99 5-2.947850313E+05 *S100393 *S100393 99 2-1.958337305E+04 *S100394 *S100394 99 6-7.005862500E+04 *S100395 DMIG AEROB105 0 1 1 DMIG *AEROB105 99 3 *D100400 *D100400 99 3 1.813275218E+00 *D100401 *D100401 99 5-6.486909389E+00 *D100402 *D100402 99 2-4.372470379E-01 *D100403 *D100403 99 6 2.729491043E+01 *D100404 DMIG *AEROB105 99 5 *D100405 *D100405 99 3 0.000000000E+00 *D100406 *D100406 99 5 5.822657471E+02 *D100407 *D100407 99 2 2.729491043E+01 *D100408 *D100408 99 6-5.249324375E+05 *D100409 DMIG *AEROB105 99 2 *D100410 *D100410 99 3 4.372470379E-01 *D100411 *D100411 99 5 2.729491043E+01 *D100412 *D100412 99 2 1.813275218E+00 *D100413 *D100413 99 6 6.486909389E+00 *D100414 DMIG *AEROB105 99 6 *D100415 *D100415 99 3 2.729491043E+01 *D100416 *D100416 99 5 5.249324375E+05 *D100417 *D100417 99 2 0.000000000E+00 *D100418 *D100418 99 6 5.822657471E+02 *D100419 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS106 AND AEROB106) ARE BASED ON $ VELOCITY = 1.000000E+03(ft/sec) $ MACH NO = 1.000000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS106 0 1 1 DMIG *AEROS106 99 3 *S100420 *S100420 1 3-6.343822861E+01 *S100421 *S100421 2 3 6.343852997E+01 *S100422 *S100422 3 3-4.893752670E+01 *S100423 *S100423 4 3 5.001690674E+01 *S100424 *S100424 5 3-5.615013504E+01 *S100425 *S100425 6 3 5.615038681E+01 *S100426 *S100426 7 3-4.220420837E+01 *S100427 *S100427 8 3 4.220441818E+01 *S100428 *S100428 9 3-2.784289742E+01 *S100429 *S100429 10 3 2.784301567E+01 *S100430 *S100430 99 3-1.079176188E+00 *S100431 *S100431 99 5 0.000000000E+00 *S100432 *S100432 99 2 0.000000000E+00 *S100433 *S100433 99 6 0.000000000E+00 *S100434 DMIG *AEROS106 99 5 *S100435 *S100435 1 3 2.000812988E+02 *S100436 *S100436 2 3-2.000822601E+02 *S100437 *S100437 3 3 1.543467407E+02 *S100438 *S100438 4 3-1.577510529E+02 *S100439 *S100439 5 3 1.770949860E+02 *S100440 *S100440 6 3-1.770957794E+02 *S100441 *S100441 7 3 1.331101685E+02 *S100442 *S100442 8 3-1.331108246E+02 *S100443 *S100443 9 3 8.781523895E+01 *S100444 *S100444 10 3-8.781561279E+01 *S100445 *S100445 99 3 2.509646875E+04 *S100446 *S100446 99 5-7.914239063E+04 *S100447 *S100447 99 2-5.888280762E+03 *S100448 *S100448 99 6 3.418331563E+05 *S100449 DMIG *AEROS106 99 2 *S100450 *S100450 1 3 1.488626862E+01 *S100451 *S100451 2 3-1.488634014E+01 *S100452 *S100452 3 3 1.148356724E+01 *S100453 *S100453 4 3-1.173685169E+01 *S100454 *S100454 5 3 1.317606163E+01 *S100455 *S100455 6 3-1.317612076E+01 *S100456 *S100456 7 3 9.903542519E+00 *S100457 *S100457 8 3-9.903592110E+00 *S100458 *S100458 9 3 6.533550262E+00 *S100459 *S100459 10 3-6.533577919E+00 *S100460 *S100460 99 3 2.532369792E-01 *S100461 *S100461 99 5 0.000000000E+00 *S100462 *S100462 99 2 0.000000000E+00 *S100463 *S100463 99 6 0.000000000E+00 *S100464 DMIG *AEROS106 99 6 *S100465 *S100465 1 3-8.641945190E+02 *S100466 *S100466 2 3 8.641986694E+02 *S100467 *S100467 3 3-6.666571045E+02 *S100468 *S100468 4 3 6.813610229E+02 *S100469 *S100469 5 3-7.649116821E+02 *S100470 *S100470 6 3 7.649151001E+02 *S100471 *S100471 7 3-5.749317017E+02 *S100472 *S100472 8 3 5.749345703E+02 *S100473 *S100473 9 3-3.792930908E+02 *S100474 *S100474 10 3 3.792946777E+02 *S100475 *S100475 99 3-5.902981934E+03 *S100476 *S100476 99 5-3.418331563E+05 *S100477 *S100477 99 2-2.509306445E+04 *S100478 *S100478 99 6-7.914239063E+04 *S100479 DMIG AEROB106 0 1 1 DMIG *AEROB106 99 3 *D100484 *D100484 99 3 2.091088533E+00 *D100485 *D100485 99 5-6.595199585E+00 *D100486 *D100486 99 2-4.906900525E-01 *D100487 *D100487 99 6 2.848609543E+01 *D100488 DMIG *AEROB106 99 5 *D100489 *D100489 99 3 0.000000000E+00 *D100490 *D100490 99 5 5.483067627E+02 *D100491 *D100491 99 2 2.848609543E+01 *D100492 *D100492 99 6-5.249324375E+05 *D100493 DMIG *AEROB106 99 2 *D100494 *D100494 99 3 4.906900525E-01 *D100495 *D100495 99 5 2.848609543E+01 *D100496 *D100496 99 2 2.091088533E+00 *D100497 *D100497 99 6 6.595199585E+00 *D100498 DMIG *AEROB106 99 6 *D100499 *D100499 99 3 2.848609543E+01 *D100500 *D100500 99 5 5.249324375E+05 *D100501 *D100501 99 2 0.000000000E+00 *D100502 *D100502 99 6 5.483067627E+02 *D100503 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS107 AND AEROB107) ARE BASED ON $ VELOCITY = 1.100000E+03(ft/sec) $ MACH NO = 1.100000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS107 0 1 1 DMIG *AEROS107 99 3 *S100504 *S100504 1 3-7.917851257E+01 *S100505 *S100505 2 3 7.917889404E+01 *S100506 *S100506 3 3-6.107989883E+01 *S100507 *S100507 4 3 6.242709351E+01 *S100508 *S100508 5 3-7.008209991E+01 *S100509 *S100509 6 3 7.008241272E+01 *S100510 *S100510 7 3-5.267591095E+01 *S100511 *S100511 8 3 5.267617416E+01 *S100512 *S100512 9 3-3.475127411E+01 *S100513 *S100513 10 3 3.475141907E+01 *S100514 *S100514 99 3-1.346941233E+00 *S100515 *S100515 99 5 0.000000000E+00 *S100516 *S100516 99 2 0.000000000E+00 *S100517 *S100517 99 6 0.000000000E+00 *S100518 DMIG *AEROS107 99 5 *S100519 *S100519 1 3 2.219992523E+02 *S100520 *S100520 2 3-2.220003204E+02 *S100521 *S100521 3 3 1.712546997E+02 *S100522 *S100522 4 3-1.750319366E+02 *S100523 *S100523 5 3 1.964949036E+02 *S100524 *S100524 6 3-1.964957733E+02 *S100525 *S100525 7 3 1.476917572E+02 *S100526 *S100526 8 3-1.476924896E+02 *S100527 *S100527 9 3 9.743498230E+01 *S100528 *S100528 10 3-9.743539429E+01 *S100529 *S100529 99 3 3.132292969E+04 *S100530 *S100530 99 5-8.781206250E+04 *S100531 *S100531 99 2-7.147415039E+03 *S100532 *S100532 99 6 3.895730938E+05 *S100533 DMIG *AEROS107 99 2 *S100534 *S100534 1 3 1.806950760E+01 *S100535 *S100535 2 3-1.806959534E+01 *S100536 *S100536 3 3 1.393918324E+01 *S100537 *S100537 4 3-1.424662876E+01 *S100538 *S100538 5 3 1.599359512E+01 *S100539 *S100539 6 3-1.599366665E+01 *S100540 *S100540 7 3 1.202128983E+01 *S100541 *S100541 8 3-1.202134991E+01 *S100542 *S100542 9 3 7.930667400E+00 *S100543 *S100543 10 3-7.930700779E+00 *S100544 *S100544 99 3 3.073885143E-01 *S100545 *S100545 99 5 0.000000000E+00 *S100546 *S100546 99 2 0.000000000E+00 *S100547 *S100547 99 6 0.000000000E+00 *S100548 DMIG *AEROS107 99 6 *S100549 *S100549 1 3-9.848867188E+02 *S100550 *S100550 2 3 9.848914795E+02 *S100551 *S100551 3 3-7.597614746E+02 *S100552 *S100552 4 3 7.765189819E+02 *S100553 *S100553 5 3-8.717381592E+02 *S100554 *S100554 6 3 8.717420654E+02 *S100555 *S100555 7 3-6.552258301E+02 *S100556 *S100556 8 3 6.552291260E+02 *S100557 *S100557 9 3-4.322646179E+02 *S100558 *S100558 10 3 4.322664185E+02 *S100559 *S100559 99 3-7.164169434E+03 *S100560 *S100560 99 5-3.895730938E+05 *S100561 *S100561 99 2-3.131915234E+04 *S100562 *S100562 99 6-8.781206250E+04 *S100563 DMIG AEROB107 0 1 1 DMIG *AEROB107 99 3 *D100568 *D100568 99 3 2.372663260E+00 *D100569 *D100569 99 5-6.652429581E+00 *D100570 *D100570 99 2-5.414708853E-01 *D100571 *D100571 99 6 2.951311493E+01 *D100572 DMIG *AEROB107 99 5 *D100573 *D100573 99 3 0.000000000E+00 *D100574 *D100574 99 5 5.174942017E+02 *D100575 *D100575 99 2 2.951311684E+01 *D100576 *D100576 99 6-5.249324375E+05 *D100577 DMIG *AEROB107 99 2 *D100578 *D100578 99 3 5.414708853E-01 *D100579 *D100579 99 5 2.951311493E+01 *D100580 *D100580 99 2 2.372663260E+00 *D100581 *D100581 99 6 6.652429581E+00 *D100582 DMIG *AEROB107 99 6 *D100583 *D100583 99 3 2.951311684E+01 *D100584 *D100584 99 5 5.249324375E+05 *D100585 *D100585 99 2 0.000000000E+00 *D100586 *D100586 99 6 5.174942017E+02 *D100587 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS108 AND AEROB108) ARE BASED ON $ VELOCITY = 1.200000E+03(ft/sec) $ MACH NO = 1.200000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS108 0 1 1 DMIG *AEROS108 99 3 *S100588 *S100588 1 3-9.673359680E+01 *S100589 *S100589 2 3 9.673406219E+01 *S100590 *S100590 3 3-7.462224579E+01 *S100591 *S100591 4 3 7.626813507E+01 *S100592 *S100592 5 3-8.562036896E+01 *S100593 *S100593 6 3 8.562075043E+01 *S100594 *S100594 7 3-6.435496521E+01 *S100595 *S100595 8 3 6.435528564E+01 *S100596 *S100596 9 3-4.245616150E+01 *S100597 *S100597 10 3 4.245634079E+01 *S100598 *S100598 99 3-1.645578623E+00 *S100599 *S100599 99 5 0.000000000E+00 *S100600 *S100600 99 2 0.000000000E+00 *S100601 *S100601 99 6 0.000000000E+00 *S100602 DMIG *AEROS108 99 5 *S100603 *S100603 1 3 2.428427887E+02 *S100604 *S100604 2 3-2.428439636E+02 *S100605 *S100605 3 3 1.873338318E+02 *S100606 *S100606 4 3-1.914657135E+02 *S100607 *S100607 5 3 2.149438324E+02 *S100608 *S100608 6 3-2.149447937E+02 *S100609 *S100609 7 3 1.615585480E+02 *S100610 *S100610 8 3-1.615593567E+02 *S100611 *S100611 9 3 1.065831680E+02 *S100612 *S100612 10 3-1.065836182E+02 *S100613 *S100613 99 3 3.826721875E+04 *S100614 *S100614 99 5-9.605675000E+04 *S100615 *S100615 99 2-8.490336914E+03 *S100616 *S100616 99 6 4.378386563E+05 *S100617 DMIG *AEROS108 99 2 *S100618 *S100618 1 3 2.146457291E+01 *S100619 *S100619 2 3-2.146467590E+01 *S100620 *S100620 3 3 1.655820465E+01 *S100621 *S100621 4 3-1.692341614E+01 *S100622 *S100622 5 3 1.899861908E+01 *S100623 *S100623 6 3-1.899870300E+01 *S100624 *S100624 7 3 1.427995968E+01 *S100625 *S100625 8 3-1.428003120E+01 *S100626 *S100626 9 3 9.420753479E+00 *S100627 *S100627 10 3-9.420793533E+00 *S100628 *S100628 99 3 3.651434779E-01 *S100629 *S100629 99 5 0.000000000E+00 *S100630 *S100630 99 2 0.000000000E+00 *S100631 *S100631 99 6 0.000000000E+00 *S100632 DMIG *AEROS108 99 6 *S100633 *S100633 1 3-1.106907715E+03 *S100634 *S100634 2 3 1.106913086E+03 *S100635 *S100635 3 3-8.538909912E+02 *S100636 *S100636 4 3 8.727246094E+02 *S100637 *S100637 5 3-9.797408447E+02 *S100638 *S100638 6 3 9.797451782E+02 *S100639 *S100639 7 3-7.364040527E+02 *S100640 *S100640 8 3 7.364077148E+02 *S100641 *S100641 9 3-4.858193665E+02 *S100642 *S100642 10 3 4.858214111E+02 *S100643 *S100643 99 3-8.509166992E+03 *S100644 *S100644 99 5-4.378386563E+05 *S100645 *S100645 99 2-3.826308594E+04 *S100646 *S100646 99 6-9.605675000E+04 *S100647 DMIG AEROB108 0 1 1 DMIG *AEROB108 99 3 *D100652 *D100652 99 3 2.657158852E+00 *D100653 *D100653 99 5-6.670608044E+00 *D100654 *D100654 99 2-5.896067619E-01 *D100655 *D100655 99 6 3.040546227E+01 *D100656 DMIG *AEROB108 99 5 *D100657 *D100657 99 3 0.000000000E+00 *D100658 *D100658 99 5 4.895316467E+02 *D100659 *D100659 99 2 3.040546227E+01 *D100660 *D100660 99 6-5.249324375E+05 *D100661 DMIG *AEROB108 99 2 *D100662 *D100662 99 3 5.896067619E-01 *D100663 *D100663 99 5 3.040546227E+01 *D100664 *D100664 99 2 2.657158852E+00 *D100665 *D100665 99 6 6.670608044E+00 *D100666 DMIG *AEROB108 99 6 *D100667 *D100667 99 3 3.040546227E+01 *D100668 *D100668 99 5 5.249324375E+05 *D100669 *D100669 99 2 0.000000000E+00 *D100670 *D100670 99 6 4.895316467E+02 *D100671 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS109 AND AEROB109) ARE BASED ON $ VELOCITY = 1.300000E+03(ft/sec) $ MACH NO = 1.300000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS109 0 1 1 DMIG *AEROS109 99 3 *S100672 *S100672 1 3-1.161054459E+02 *S100673 *S100673 2 3 1.161060028E+02 *S100674 *S100674 3 3-8.956608582E+01 *S100675 *S100675 4 3 9.154157257E+01 *S100676 *S100676 5 3-1.027666855E+02 *S100677 *S100677 6 3 1.027671509E+02 *S100678 *S100678 7 3-7.724267578E+01 *S100679 *S100679 8 3 7.724306488E+01 *S100680 *S100680 9 3-5.095842361E+01 *S100681 *S100681 10 3 5.095863724E+01 *S100682 *S100682 99 3-1.975121856E+00 *S100683 *S100683 99 5 0.000000000E+00 *S100684 *S100684 99 2 0.000000000E+00 *S100685 *S100685 99 6 0.000000000E+00 *S100686 DMIG *AEROS109 99 5 *S100687 *S100687 1 3 2.626255493E+02 *S100688 *S100688 2 3-2.626268005E+02 *S100689 *S100689 3 3 2.025946350E+02 *S100690 *S100690 4 3-2.070631104E+02 *S100691 *S100691 5 3 2.324538422E+02 *S100692 *S100692 6 3-2.324548798E+02 *S100693 *S100693 7 3 1.747196198E+02 *S100694 *S100694 8 3-1.747204895E+02 *S100695 *S100695 9 3 1.152657700E+02 *S100696 *S100696 10 3-1.152662506E+02 *S100697 *S100697 99 3 4.593011328E+04 *S100698 *S100698 99 5-1.038818359E+05 *S100699 *S100699 99 2-9.908916992E+03 *S100700 *S100700 99 6 4.865081875E+05 *S100701 DMIG *AEROS109 99 2 *S100702 *S100702 1 3 2.505091095E+01 *S100703 *S100703 2 3-2.505103111E+01 *S100704 *S100704 3 3 1.932477760E+01 *S100705 *S100705 4 3-1.975100899E+01 *S100706 *S100706 5 3 2.217294121E+01 *S100707 *S100707 6 3-2.217304039E+01 *S100708 *S100708 7 3 1.666588020E+01 *S100709 *S100709 8 3-1.666596413E+01 *S100710 *S100710 9 3 1.099479008E+01 *S100711 *S100711 10 3-1.099483585E+01 *S100712 *S100712 99 3 4.261522889E-01 *S100713 *S100713 99 5 0.000000000E+00 *S100714 *S100714 99 2 0.000000000E+00 *S100715 *S100715 99 6 0.000000000E+00 *S100716 DMIG *AEROS109 99 6 *S100717 *S100717 1 3-1.229950073E+03 *S100718 *S100718 2 3 1.229955933E+03 *S100719 *S100719 3 3-9.488082886E+02 *S100720 *S100720 4 3 9.697354126E+02 *S100721 *S100721 5 3-1.088647461E+03 *S100722 *S100722 6 3 1.088652344E+03 *S100723 *S100723 7 3-8.182617188E+02 *S100724 *S100724 8 3 8.182657471E+02 *S100725 *S100725 9 3-5.398223877E+02 *S100726 *S100726 10 3 5.398246460E+02 *S100727 *S100727 99 3-9.929839844E+03 *S100728 *S100728 99 5-4.865081875E+05 *S100729 *S100729 99 2-4.592564453E+04 *S100730 *S100730 99 6-1.038818359E+05 *S100731 DMIG AEROB109 0 1 1 DMIG *AEROB109 99 3 *D100736 *D100736 99 3 2.943951607E+00 *D100737 *D100737 99 5-6.659091473E+00 *D100738 *D100738 99 2-6.351869702E-01 *D100739 *D100739 99 6 3.118642044E+01 *D100740 DMIG *AEROB109 99 5 *D100741 *D100741 99 3 0.000000000E+00 *D100742 *D100742 99 5 4.641217957E+02 *D100743 *D100743 99 2 3.118642044E+01 *D100744 *D100744 99 6-5.249324375E+05 *D100745 DMIG *AEROB109 99 2 *D100746 *D100746 99 3 6.351869702E-01 *D100747 *D100747 99 5 3.118642044E+01 *D100748 *D100748 99 2 2.943951607E+00 *D100749 *D100749 99 6 6.659091473E+00 *D100750 DMIG *AEROB109 99 6 *D100751 *D100751 99 3 3.118642044E+01 *D100752 *D100752 99 5 5.249324375E+05 *D100753 *D100753 99 2 0.000000000E+00 *D100754 *D100754 99 6 4.641217957E+02 *D100755 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS110 AND AEROB110) ARE BASED ON $ VELOCITY = 1.325000E+03(ft/sec) $ MACH NO = 1.325000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS110 0 1 1 DMIG *AEROS110 99 3 *S100756 *S100756 1 3-1.212323608E+02 *S100757 *S100757 2 3 1.212329407E+02 *S100758 *S100758 3 3-9.352108765E+01 *S100759 *S100759 4 3 9.558380890E+01 *S100760 *S100760 5 3-1.073045959E+02 *S100761 *S100761 6 3 1.073050766E+02 *S100762 *S100762 7 3-8.065351105E+01 *S100763 *S100763 8 3 8.065391541E+01 *S100764 *S100764 9 3-5.320861435E+01 *S100765 *S100765 10 3 5.320883942E+01 *S100766 *S100766 99 3-2.062338114E+00 *S100767 *S100767 99 5 0.000000000E+00 *S100768 *S100768 99 2 0.000000000E+00 *S100769 *S100769 99 6 0.000000000E+00 *S100770 DMIG *AEROS110 99 5 *S100771 *S100771 1 3 2.674094238E+02 *S100772 *S100772 2 3-2.674107056E+02 *S100773 *S100773 3 3 2.062850189E+02 *S100774 *S100774 4 3-2.108348999E+02 *S100775 *S100775 5 3 2.366881256E+02 *S100776 *S100776 6 3-2.366891937E+02 *S100777 *S100777 7 3 1.779022522E+02 *S100778 *S100778 8 3-1.779031372E+02 *S100779 *S100779 9 3 1.173654099E+02 *S100780 *S100780 10 3-1.173658981E+02 *S100781 *S100781 99 3 4.795815234E+04 *S100782 *S100782 99 5-1.057741094E+05 *S100783 *S100783 99 2-1.027453027E+04 *S100784 *S100784 99 6 4.987275000E+05 *S100785 DMIG *AEROS110 99 2 *S100786 *S100786 1 3 2.597522545E+01 *S100787 *S100787 2 3-2.597534943E+01 *S100788 *S100788 3 3 2.003781128E+01 *S100789 *S100789 4 3-2.047977066E+01 *S100790 *S100790 5 3 2.299106407E+01 *S100791 *S100791 6 3-2.299116707E+01 *S100792 *S100792 7 3 1.728080750E+01 *S100793 *S100793 8 3-1.728089333E+01 *S100794 *S100794 9 3 1.140046883E+01 *S100795 *S100795 10 3-1.140051651E+01 *S100796 *S100796 99 3 4.418762028E-01 *S100797 *S100797 99 5 0.000000000E+00 *S100798 *S100798 99 2 0.000000000E+00 *S100799 *S100799 99 6 0.000000000E+00 *S100800 DMIG *AEROS110 99 6 *S100801 *S100801 1 3-1.260841919E+03 *S100802 *S100802 2 3 1.260848022E+03 *S100803 *S100803 3 3-9.726389160E+02 *S100804 *S100804 4 3 9.940916748E+02 *S100805 *S100805 5 3-1.115990356E+03 *S100806 *S100806 6 3 1.115995239E+03 *S100807 *S100807 7 3-8.388134155E+02 *S100808 *S100808 8 3 8.388176270E+02 *S100809 *S100809 9 3-5.533807373E+02 *S100810 *S100810 10 3 5.533830566E+02 *S100811 *S100811 99 3-1.029597949E+04 *S100812 *S100812 99 5-4.987275000E+05 *S100813 *S100813 99 2-4.795360156E+04 *S100814 *S100814 99 6-1.057741094E+05 *S100815 DMIG AEROB110 0 1 1 DMIG *AEROB110 99 3 *D100820 *D100820 99 3 3.015950441E+00 *D100821 *D100821 99 5-6.652460575E+00 *D100822 *D100822 99 2-6.461970210E-01 *D100823 *D100823 99 6 3.136651421E+01 *D100824 DMIG *AEROB110 99 5 *D100825 *D100825 99 3 0.000000000E+00 *D100826 *D100826 99 5 4.581349182E+02 *D100827 *D100827 99 2 3.136651421E+01 *D100828 *D100828 99 6-5.249324375E+05 *D100829 DMIG *AEROB110 99 2 *D100830 *D100830 99 3 6.461970210E-01 *D100831 *D100831 99 5 3.136651421E+01 *D100832 *D100832 99 2 3.015950441E+00 *D100833 *D100833 99 6 6.652460575E+00 *D100834 DMIG *AEROB110 99 6 *D100835 *D100835 99 3 3.136651421E+01 *D100836 *D100836 99 5 5.249324375E+05 *D100837 *D100837 99 2 0.000000000E+00 *D100838 *D100838 99 6 4.581349182E+02 *D100839 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS111 AND AEROB111) ARE BASED ON $ VELOCITY = 1.350000E+03(ft/sec) $ MACH NO = 1.350000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS111 0 1 1 DMIG *AEROS111 99 3 *S100840 *S100840 1 3-1.264729004E+02 *S100841 *S100841 2 3 1.264735107E+02 *S100842 *S100842 3 3-9.756374359E+01 *S100843 *S100843 4 3 9.971563721E+01 *S100844 *S100844 5 3-1.119430847E+02 *S100845 *S100845 6 3 1.119435806E+02 *S100846 *S100846 7 3-8.413994598E+01 *S100847 *S100847 8 3 8.414036560E+01 *S100848 *S100848 9 3-5.550867844E+01 *S100849 *S100849 10 3 5.550891113E+01 *S100850 *S100850 99 3-2.151487350E+00 *S100851 *S100851 99 5 0.000000000E+00 *S100852 *S100852 99 2 0.000000000E+00 *S100853 *S100853 99 6 0.000000000E+00 *S100854 DMIG *AEROS111 99 5 *S100855 *S100855 1 3 2.721300659E+02 *S100856 *S100856 2 3-2.721313782E+02 *S100857 *S100857 3 3 2.099266205E+02 *S100858 *S100858 4 3-2.145568237E+02 *S100859 *S100859 5 3 2.408664551E+02 *S100860 *S100860 6 3-2.408675232E+02 *S100861 *S100861 7 3 1.810428009E+02 *S100862 *S100862 8 3-1.810437012E+02 *S100863 *S100863 9 3 1.194372864E+02 *S100864 *S100864 10 3-1.194377899E+02 *S100865 *S100865 99 3 5.003113281E+04 *S100866 *S100866 99 5-1.076413672E+05 *S100867 *S100867 99 2-1.064432520E+04 *S100868 *S100868 99 6 5.109651875E+05 *S100869 DMIG *AEROS111 99 2 *S100870 *S100870 1 3 2.691011047E+01 *S100871 *S100871 2 3-2.691023827E+01 *S100872 *S100872 3 3 2.075900078E+01 *S100873 *S100873 4 3-2.121686745E+01 *S100874 *S100874 5 3 2.381854630E+01 *S100875 *S100875 6 3-2.381865120E+01 *S100876 *S100876 7 3 1.790276909E+01 *S100877 *S100877 8 3-1.790285873E+01 *S100878 *S100878 9 3 1.181078815E+01 *S100879 *S100879 10 3-1.181083775E+01 *S100880 *S100880 99 3 4.577799439E-01 *S100881 *S100881 99 5 0.000000000E+00 *S100882 *S100882 99 2 0.000000000E+00 *S100883 *S100883 99 6 0.000000000E+00 *S100884 DMIG *AEROS111 99 6 *S100885 *S100885 1 3-1.291780273E+03 *S100886 *S100886 2 3 1.291786499E+03 *S100887 *S100887 3 3-9.965053101E+02 *S100888 *S100888 4 3 1.018484497E+03 *S100889 *S100889 5 3-1.143374268E+03 *S100890 *S100890 6 3 1.143379395E+03 *S100891 *S100891 7 3-8.593961182E+02 *S100892 *S100892 8 3 8.594003906E+02 *S100893 *S100893 9 3-5.669595337E+02 *S100894 *S100894 10 3 5.669619141E+02 *S100895 *S100895 99 3-1.066629980E+04 *S100896 *S100896 99 5-5.109651875E+05 *S100897 *S100897 99 2-5.002650391E+04 *S100898 *S100898 99 6-1.076413672E+05 *S100899 DMIG AEROB111 0 1 1 DMIG *AEROB111 99 3 *D100904 *D100904 99 3 3.088055849E+00 *D100905 *D100905 99 5-6.644528866E+00 *D100906 *D100906 99 2-6.570571661E-01 *D100907 *D100907 99 6 3.154106140E+01 *D100908 DMIG *AEROB111 99 5 *D100909 *D100909 99 3 0.000000000E+00 *D100910 *D100910 99 5 4.522857971E+02 *D100911 *D100911 99 2 3.154105949E+01 *D100912 *D100912 99 6-5.249324375E+05 *D100913 DMIG *AEROB111 99 2 *D100914 *D100914 99 3 6.570571661E-01 *D100915 *D100915 99 5 3.154106140E+01 *D100916 *D100916 99 2 3.088055849E+00 *D100917 *D100917 99 6 6.644528866E+00 *D100918 DMIG *AEROB111 99 6 *D100919 *D100919 99 3 3.154105949E+01 *D100920 *D100920 99 5 5.249324375E+05 *D100921 *D100921 99 2 0.000000000E+00 *D100922 *D100922 99 6 4.522857971E+02 *D100923 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS112 AND AEROB112) ARE BASED ON $ VELOCITY = 1.400000E+03(ft/sec) $ MACH NO = 1.400000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS112 0 1 1 DMIG *AEROS112 99 3 *S100924 *S100924 1 3-1.372948456E+02 *S100925 *S100925 2 3 1.372955017E+02 *S100926 *S100926 3 3-1.059120026E+02 *S100927 *S100927 4 3 1.082480240E+02 *S100928 *S100928 5 3-1.215217361E+02 *S100929 *S100929 6 3 1.215222855E+02 *S100930 *S100930 7 3-9.133956146E+01 *S100931 *S100931 8 3 9.134001923E+01 *S100932 *S100932 9 3-6.025839996E+01 *S100933 *S100933 10 3 6.025865555E+01 *S100934 *S100934 99 3-2.335584164E+00 *S100935 *S100935 99 5 0.000000000E+00 *S100936 *S100936 99 2 0.000000000E+00 *S100937 *S100937 99 6 0.000000000E+00 *S100938 DMIG *AEROS112 99 5 *S100939 *S100939 1 3 2.813847351E+02 *S100940 *S100940 2 3-2.813860779E+02 *S100941 *S100941 3 3 2.170658569E+02 *S100942 *S100942 4 3-2.218535156E+02 *S100943 *S100943 5 3 2.490578918E+02 *S100944 *S100944 6 3-2.490590057E+02 *S100945 *S100945 7 3 1.871997528E+02 *S100946 *S100946 8 3-1.872006836E+02 *S100947 *S100947 9 3 1.234991455E+02 *S100948 *S100948 10 3-1.234996643E+02 *S100949 *S100949 99 3 5.431191797E+04 *S100950 *S100950 99 5-1.113020625E+05 *S100951 *S100951 99 2-1.139608203E+04 *S100952 *S100952 99 6 5.354912500E+05 *S100953 DMIG *AEROS112 99 2 *S100954 *S100954 1 3 2.881064034E+01 *S100955 *S100955 2 3-2.881077766E+01 *S100956 *S100956 3 3 2.222510910E+01 *S100957 *S100957 4 3-2.271531105E+01 *S100958 *S100958 5 3 2.550073242E+01 *S100959 *S100959 6 3-2.550084686E+01 *S100960 *S100960 7 3 1.916715431E+01 *S100961 *S100961 8 3-1.916724968E+01 *S100962 *S100962 9 3 1.264492607E+01 *S100963 *S100963 10 3-1.264497948E+01 *S100964 *S100964 99 3 4.901107252E-01 *S100965 *S100965 99 5 0.000000000E+00 *S100966 *S100966 99 2 0.000000000E+00 *S100967 *S100967 99 6 0.000000000E+00 *S100968 DMIG *AEROS112 99 6 *S100969 *S100969 1 3-1.353785034E+03 *S100970 *S100970 2 3 1.353791504E+03 *S100971 *S100971 3 3-1.044337036E+03 *S100972 *S100972 4 3 1.067371216E+03 *S100973 *S100973 5 3-1.198255615E+03 *S100974 *S100974 6 3 1.198260986E+03 *S100975 *S100975 7 3-9.006466675E+02 *S100976 *S100976 8 3 9.006511230E+02 *S100977 *S100977 9 3-5.941732788E+02 *S100978 *S100978 10 3 5.941757813E+02 *S100979 *S100979 99 3-1.141911230E+04 *S100980 *S100980 99 5-5.354912500E+05 *S100981 *S100981 99 2-5.430713281E+04 *S100982 *S100982 99 6-1.113020625E+05 *S100983 DMIG AEROB112 0 1 1 DMIG *AEROB112 99 3 *D100988 *D100988 99 3 3.232567549E+00 *D100989 *D100989 99 5-6.625123024E+00 *D100990 *D100990 99 2-6.783382297E-01 *D100991 *D100991 99 6 3.187448311E+01 *D100992 DMIG *AEROB112 99 5 *D100993 *D100993 99 3 0.000000000E+00 *D100994 *D100994 99 5 4.409851379E+02 *D100995 *D100995 99 2 3.187448502E+01 *D100996 *D100996 99 6-5.249324375E+05 *D100997 DMIG *AEROB112 99 2 *D100998 *D100998 99 3 6.783382297E-01 *D100999 *D100999 99 5 3.187448311E+01 *D101000 *D101000 99 2 3.232567549E+00 *D101001 *D101001 99 6 6.625123024E+00 *D101002 DMIG *AEROB112 99 6 *D101003 *D101003 99 3 3.187448502E+01 *D101004 *D101004 99 5 5.249324375E+05 *D101005 *D101005 99 2 0.000000000E+00 *D101006 *D101006 99 6 4.409851379E+02 *D101007 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS113 AND AEROB113) ARE BASED ON $ VELOCITY = 1.500000E+03(ft/sec) $ MACH NO = 1.500000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS113 0 1 1 DMIG *AEROS113 99 3 *S101008 *S101008 1 3-1.603019104E+02 *S101009 *S101009 2 3 1.603026886E+02 *S101010 *S101010 3 3-1.236601334E+02 *S101011 *S101011 4 3 1.263876114E+02 *S101012 *S101012 5 3-1.418856506E+02 *S101013 *S101013 6 3 1.418862915E+02 *S101014 *S101014 7 3-1.066457214E+02 *S101015 *S101015 8 3 1.066462555E+02 *S101016 *S101016 9 3-7.035615540E+01 *S101017 *S101017 10 3 7.035645294E+01 *S101018 *S101018 99 3-2.726967812E+00 *S101019 *S101019 99 5 0.000000000E+00 *S101020 *S101020 99 2 0.000000000E+00 *S101021 *S101021 99 6 0.000000000E+00 *S101022 DMIG *AEROS113 99 5 *S101023 *S101023 1 3 2.991712036E+02 *S101024 *S101024 2 3-2.991726379E+02 *S101025 *S101025 3 3 2.307866974E+02 *S101026 *S101026 4 3-2.358769836E+02 *S101027 *S101027 5 3 2.648009644E+02 *S101028 *S101028 6 3-2.648021545E+02 *S101029 *S101029 7 3 1.990327301E+02 *S101030 *S101030 8 3-1.990337219E+02 *S101031 *S101031 9 3 1.313055725E+02 *S101032 *S101032 10 3-1.313061371E+02 *S101033 *S101033 99 3 6.341269922E+04 *S101034 *S101034 99 5-1.183375156E+05 *S101035 *S101035 99 2-1.294570801E+04 *S101036 *S101036 99 6 5.847203125E+05 *S101037 DMIG *AEROS113 99 2 *S101038 *S101038 1 3 3.272827530E+01 *S101039 *S101039 2 3-3.272843552E+01 *S101040 *S101040 3 3 2.524725342E+01 *S101041 *S101041 4 3-2.580411148E+01 *S101042 *S101042 5 3 2.896829414E+01 *S101043 *S101043 6 3-2.896842384E+01 *S101044 *S101044 7 3 2.177348137E+01 *S101045 *S101045 8 3-2.177359009E+01 *S101046 *S101046 9 3 1.436436844E+01 *S101047 *S101047 10 3-1.436442852E+01 *S101048 *S101048 99 3 5.567554235E-01 *S101049 *S101049 99 5 0.000000000E+00 *S101050 *S101050 99 2 0.000000000E+00 *S101051 *S101051 99 6 0.000000000E+00 *S101052 DMIG *AEROS113 99 6 *S101053 *S101053 1 3-1.478241943E+03 *S101054 *S101054 2 3 1.478249023E+03 *S101055 *S101055 3 3-1.140345581E+03 *S101056 *S101056 4 3 1.165497314E+03 *S101057 *S101057 5 3-1.308414307E+03 *S101058 *S101058 6 3 1.308420166E+03 *S101059 *S101059 7 3-9.834453735E+02 *S101060 *S101060 8 3 9.834502563E+02 *S101061 *S101061 9 3-6.487971191E+02 *S101062 *S101062 10 3 6.487998657E+02 *S101063 *S101063 99 3-1.297085547E+04 *S101064 *S101064 99 5-5.847203125E+05 *S101065 *S101065 99 2-6.340760938E+04 *S101066 *S101066 99 6-1.183375156E+05 *S101067 DMIG AEROB113 0 1 1 DMIG *AEROB113 99 3 *D101072 *D101072 99 3 3.522644997E+00 *D101073 *D101073 99 5-6.574306488E+00 *D101074 *D101074 99 2-7.192059755E-01 *D101075 *D101075 99 6 3.248446274E+01 *D101076 DMIG *AEROB113 99 5 *D101077 *D101077 99 3 0.000000000E+00 *D101078 *D101078 99 5 4.198679810E+02 *D101079 *D101079 99 2 3.248446274E+01 *D101080 *D101080 99 6-5.249324375E+05 *D101081 DMIG *AEROB113 99 2 *D101082 *D101082 99 3 7.192059755E-01 *D101083 *D101083 99 5 3.248446274E+01 *D101084 *D101084 99 2 3.522644997E+00 *D101085 *D101085 99 6 6.574306488E+00 *D101086 DMIG *AEROB113 99 6 *D101087 *D101087 99 3 3.248446274E+01 *D101088 *D101088 99 5 5.249324375E+05 *D101089 *D101089 99 2 0.000000000E+00 *D101090 *D101090 99 6 4.198679810E+02 *D101091 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS114 AND AEROB114) ARE BASED ON $ VELOCITY = 1.600000E+03(ft/sec) $ MACH NO = 1.600000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS114 0 1 1 DMIG *AEROS114 99 3 *S101092 *S101092 1 3-1.851263733E+02 *S101093 *S101093 2 3 1.851272583E+02 *S101094 *S101094 3 3-1.428102112E+02 *S101095 *S101095 4 3 1.459600677E+02 *S101096 *S101096 5 3-1.638581543E+02 *S101097 *S101097 6 3 1.638588867E+02 *S101098 *S101098 7 3-1.231609497E+02 *S101099 *S101099 8 3 1.231615601E+02 *S101100 *S101100 9 3-8.125155640E+01 *S101101 *S101101 10 3 8.125189972E+01 *S101102 *S101102 99 3-3.149267912E+00 *S101103 *S101103 99 5 0.000000000E+00 *S101104 *S101104 99 2 0.000000000E+00 *S101105 *S101105 99 6 0.000000000E+00 *S101106 DMIG *AEROS114 99 5 *S101107 *S101107 1 3 3.160418396E+02 *S101108 *S101108 2 3-3.160433350E+02 *S101109 *S101109 3 3 2.438010406E+02 *S101110 *S101110 4 3-2.491783752E+02 *S101111 *S101111 5 3 2.797333984E+02 *S101112 *S101112 6 3-2.797346497E+02 *S101113 *S101113 7 3 2.102564392E+02 *S101114 *S101114 8 3-2.102574768E+02 *S101115 *S101115 9 3 1.387100525E+02 *S101116 *S101116 10 3-1.387106476E+02 *S101117 *S101117 99 3 7.323232813E+04 *S101118 *S101118 99 5-1.250107109E+05 *S101119 *S101119 99 2-1.455246387E+04 *S101120 *S101120 99 6 6.341431875E+05 *S101121 DMIG *AEROS114 99 2 *S101122 *S101122 1 3 3.679034424E+01 *S101123 *S101123 2 3-3.679051971E+01 *S101124 *S101124 3 3 2.838081360E+01 *S101125 *S101125 4 3-2.900678825E+01 *S101126 *S101126 5 3 3.256369019E+01 *S101127 *S101127 6 3-3.256383896E+01 *S101128 *S101128 7 3 2.447589493E+01 *S101129 *S101129 8 3-2.447601700E+01 *S101130 *S101130 9 3 1.614720154E+01 *S101131 *S101131 10 3-1.614726830E+01 *S101132 *S101132 99 3 6.258570552E-01 *S101133 *S101133 99 5 0.000000000E+00 *S101134 *S101134 99 2 0.000000000E+00 *S101135 *S101135 99 6 0.000000000E+00 *S101136 DMIG *AEROS114 99 6 *S101137 *S101137 1 3-1.603188843E+03 *S101138 *S101138 2 3 1.603196411E+03 *S101139 *S101139 3 3-1.236732178E+03 *S101140 *S101140 4 3 1.264009766E+03 *S101141 *S101141 5 3-1.419006714E+03 *S101142 *S101142 6 3 1.419013062E+03 *S101143 *S101143 7 3-1.066570068E+03 *S101144 *S101144 8 3 1.066575439E+03 *S101145 *S101145 9 3-7.036360474E+02 *S101146 *S101146 10 3 7.036389771E+02 *S101147 *S101147 99 3-1.457973633E+04 *S101148 *S101148 99 5-6.341431875E+05 *S101149 *S101149 99 2-7.322695313E+04 *S101150 *S101150 99 6-1.250107109E+05 *S101151 DMIG AEROB114 0 1 1 DMIG *AEROB114 99 3 *D101156 *D101156 99 3 3.813903570E+00 *D101157 *D101157 99 5-6.510973930E+00 *D101158 *D101158 99 2-7.579407692E-01 *D101159 *D101159 99 6 3.302828598E+01 *D101160 DMIG *AEROB114 99 5 *D101161 *D101161 99 3 0.000000000E+00 *D101162 *D101162 99 5 4.005439453E+02 *D101163 *D101163 99 2 3.302828979E+01 *D101164 *D101164 99 6-5.249324375E+05 *D101165 DMIG *AEROB114 99 2 *D101166 *D101166 99 3 7.579407692E-01 *D101167 *D101167 99 5 3.302828598E+01 *D101168 *D101168 99 2 3.813903570E+00 *D101169 *D101169 99 6 6.510973930E+00 *D101170 DMIG *AEROB114 99 6 *D101171 *D101171 99 3 3.302828979E+01 *D101172 *D101172 99 5 5.249324375E+05 *D101173 *D101173 99 2 0.000000000E+00 *D101174 *D101174 99 6 4.005439453E+02 *D101175 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS115 AND AEROB115) ARE BASED ON $ VELOCITY = 1.700000E+03(ft/sec) $ MACH NO = 1.700000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS115 0 1 1 DMIG *AEROS115 99 3 *S101176 *S101176 1 3-2.117675323E+02 *S101177 *S101177 2 3 2.117685394E+02 *S101178 *S101178 3 3-1.633617401E+02 *S101179 *S101179 4 3 1.669648895E+02 *S101180 *S101180 5 3-1.874386444E+02 *S101181 *S101181 6 3 1.874394836E+02 *S101182 *S101182 7 3-1.408847809E+02 *S101183 *S101183 8 3 1.408854828E+02 *S101184 *S101184 9 3-9.294429779E+01 *S101185 *S101185 10 3 9.294468689E+01 *S101186 *S101186 99 3-3.602472305E+00 *S101187 *S101187 99 5 0.000000000E+00 *S101188 *S101188 99 2 0.000000000E+00 *S101189 *S101189 99 6 0.000000000E+00 *S101190 DMIG *AEROS115 99 5 *S101191 *S101191 1 3 3.320554199E+02 *S101192 *S101192 2 3-3.320570068E+02 *S101193 *S101193 3 3 2.561542358E+02 *S101194 *S101194 4 3-2.618040466E+02 *S101195 *S101195 5 3 2.939072876E+02 *S101196 *S101196 6 3-2.939085999E+02 *S101197 *S101197 7 3 2.209099579E+02 *S101198 *S101198 8 3-2.209110565E+02 *S101199 *S101199 9 3 1.457383881E+02 *S101200 *S101200 10 3-1.457389984E+02 *S101201 *S101201 99 3 8.377053906E+04 *S101202 *S101202 99 5-1.313449063E+05 *S101203 *S101203 99 2-1.621171777E+04 *S101204 *S101204 99 6 6.837201875E+05 *S101205 DMIG *AEROS115 99 2 *S101206 *S101206 1 3 4.098513412E+01 *S101207 *S101207 2 3-4.098533249E+01 *S101208 *S101208 3 3 3.161675835E+01 *S101209 *S101209 4 3-3.231410599E+01 *S101210 *S101210 5 3 3.627656174E+01 *S101211 *S101211 6 3-3.627672577E+01 *S101212 *S101212 7 3 2.726660728E+01 *S101213 *S101213 8 3-2.726674271E+01 *S101214 *S101214 9 3 1.798828506E+01 *S101215 *S101215 10 3-1.798836136E+01 *S101216 *S101216 99 3 6.972165108E-01 *S101217 *S101217 99 5 0.000000000E+00 *S101218 *S101218 99 2 0.000000000E+00 *S101219 *S101219 99 6 0.000000000E+00 *S101220 DMIG *AEROS115 99 6 *S101221 *S101221 1 3-1.728525269E+03 *S101222 *S101222 2 3 1.728533569E+03 *S101223 *S101223 3 3-1.333419312E+03 *S101224 *S101224 4 3 1.362829468E+03 *S101225 *S101225 5 3-1.529943848E+03 *S101226 *S101226 6 3 1.529950684E+03 *S101227 *S101227 7 3-1.149953979E+03 *S101228 *S101228 8 3 1.149959717E+03 *S101229 *S101229 9 3-7.586459351E+02 *S101230 *S101230 10 3 7.586491089E+02 *S101231 *S101231 99 3-1.624112207E+04 *S101232 *S101232 99 5-6.837201875E+05 *S101233 *S101233 99 2-8.376489063E+04 *S101234 *S101234 99 6-1.313449063E+05 *S101235 DMIG AEROB115 0 1 1 DMIG *AEROB115 99 3 *D101240 *D101240 99 3 4.106121540E+00 *D101241 *D101241 99 5-6.438475609E+00 *D101242 *D101242 99 2-7.946919203E-01 *D101243 *D101243 99 6 3.351569366E+01 *D101244 DMIG *AEROB115 99 5 *D101245 *D101245 99 3 0.000000000E+00 *D101246 *D101246 99 5 3.828138123E+02 *D101247 *D101247 99 2 3.351568985E+01 *D101248 *D101248 99 6-5.249324375E+05 *D101249 DMIG *AEROB115 99 2 *D101250 *D101250 99 3 7.946919203E-01 *D101251 *D101251 99 5 3.351569366E+01 *D101252 *D101252 99 2 4.106121540E+00 *D101253 *D101253 99 6 6.438475609E+00 *D101254 DMIG *AEROB115 99 6 *D101255 *D101255 99 3 3.351568985E+01 *D101256 *D101256 99 5 5.249324375E+05 *D101257 *D101257 99 2 0.000000000E+00 *D101258 *D101258 99 6 3.828138123E+02 *D101259 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS116 AND AEROB116) ARE BASED ON $ VELOCITY = 1.700000E+03(ft/sec) $ MACH NO = 1.700000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS116 0 1 1 DMIG *AEROS116 99 3 *S101260 *S101260 1 3-2.117675323E+02 *S101261 *S101261 2 3 2.117685394E+02 *S101262 *S101262 3 3-1.633617401E+02 *S101263 *S101263 4 3 1.669648895E+02 *S101264 *S101264 5 3-1.874386444E+02 *S101265 *S101265 6 3 1.874394836E+02 *S101266 *S101266 7 3-1.408847809E+02 *S101267 *S101267 8 3 1.408854828E+02 *S101268 *S101268 9 3-9.294429779E+01 *S101269 *S101269 10 3 9.294468689E+01 *S101270 *S101270 99 3-3.602472305E+00 *S101271 *S101271 99 5 0.000000000E+00 *S101272 *S101272 99 2 0.000000000E+00 *S101273 *S101273 99 6 0.000000000E+00 *S101274 DMIG *AEROS116 99 5 *S101275 *S101275 1 3 3.320554199E+02 *S101276 *S101276 2 3-3.320570068E+02 *S101277 *S101277 3 3 2.561542358E+02 *S101278 *S101278 4 3-2.618040466E+02 *S101279 *S101279 5 3 2.939072876E+02 *S101280 *S101280 6 3-2.939085999E+02 *S101281 *S101281 7 3 2.209099579E+02 *S101282 *S101282 8 3-2.209110565E+02 *S101283 *S101283 9 3 1.457383881E+02 *S101284 *S101284 10 3-1.457389984E+02 *S101285 *S101285 99 3 8.377053906E+04 *S101286 *S101286 99 5-1.313449063E+05 *S101287 *S101287 99 2-1.621171777E+04 *S101288 *S101288 99 6 6.837201875E+05 *S101289 DMIG *AEROS116 99 2 *S101290 *S101290 1 3 4.098513412E+01 *S101291 *S101291 2 3-4.098533249E+01 *S101292 *S101292 3 3 3.161675835E+01 *S101293 *S101293 4 3-3.231410599E+01 *S101294 *S101294 5 3 3.627656174E+01 *S101295 *S101295 6 3-3.627672577E+01 *S101296 *S101296 7 3 2.726660728E+01 *S101297 *S101297 8 3-2.726674271E+01 *S101298 *S101298 9 3 1.798828506E+01 *S101299 *S101299 10 3-1.798836136E+01 *S101300 *S101300 99 3 6.972165108E-01 *S101301 *S101301 99 5 0.000000000E+00 *S101302 *S101302 99 2 0.000000000E+00 *S101303 *S101303 99 6 0.000000000E+00 *S101304 DMIG *AEROS116 99 6 *S101305 *S101305 1 3-1.728525269E+03 *S101306 *S101306 2 3 1.728533569E+03 *S101307 *S101307 3 3-1.333419312E+03 *S101308 *S101308 4 3 1.362829468E+03 *S101309 *S101309 5 3-1.529943848E+03 *S101310 *S101310 6 3 1.529950684E+03 *S101311 *S101311 7 3-1.149953979E+03 *S101312 *S101312 8 3 1.149959717E+03 *S101313 *S101313 9 3-7.586459351E+02 *S101314 *S101314 10 3 7.586491089E+02 *S101315 *S101315 99 3-1.624112207E+04 *S101316 *S101316 99 5-6.837201875E+05 *S101317 *S101317 99 2-8.376489063E+04 *S101318 *S101318 99 6-1.313449063E+05 *S101319 DMIG AEROB116 0 1 1 DMIG *AEROB116 99 3 *D101324 *D101324 99 3 4.106121540E+00 *D101325 *D101325 99 5-6.438475609E+00 *D101326 *D101326 99 2-7.946919203E-01 *D101327 *D101327 99 6 3.351569366E+01 *D101328 DMIG *AEROB116 99 5 *D101329 *D101329 99 3 0.000000000E+00 *D101330 *D101330 99 5 3.828138123E+02 *D101331 *D101331 99 2 3.351568985E+01 *D101332 *D101332 99 6-5.249324375E+05 *D101333 DMIG *AEROB116 99 2 *D101334 *D101334 99 3 7.946919203E-01 *D101335 *D101335 99 5 3.351569366E+01 *D101336 *D101336 99 2 4.106121540E+00 *D101337 *D101337 99 6 6.438475609E+00 *D101338 DMIG *AEROB116 99 6 *D101339 *D101339 99 3 3.351568985E+01 *D101340 *D101340 99 5 5.249324375E+05 *D101341 *D101341 99 2 0.000000000E+00 *D101342 *D101342 99 6 3.828138123E+02 *D101343 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS117 AND AEROB117) ARE BASED ON $ VELOCITY = 1.900000E+03(ft/sec) $ MACH NO = 1.900000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS117 0 1 1 DMIG *AEROS117 99 3 *S101344 *S101344 1 3-2.704964294E+02 *S101345 *S101345 2 3 2.704977112E+02 *S101346 *S101346 3 3-2.086663818E+02 *S101347 *S101347 4 3 2.132687836E+02 *S101348 *S101348 5 3-2.394204712E+02 *S101349 *S101349 6 3 2.394215393E+02 *S101350 *S101350 7 3-1.799559631E+02 *S101351 *S101351 8 3 1.799568634E+02 *S101352 *S101352 9 3-1.187202835E+02 *S101353 *S101353 10 3 1.187207794E+02 *S101354 *S101354 99 3-4.601535797E+00 *S101355 *S101355 99 5 0.000000000E+00 *S101356 *S101356 99 2 0.000000000E+00 *S101357 *S101357 99 6 0.000000000E+00 *S101358 DMIG *AEROS117 99 5 *S101359 *S101359 1 3 3.617414856E+02 *S101360 *S101360 2 3-3.617432251E+02 *S101361 *S101361 3 3 2.790546875E+02 *S101362 *S101362 4 3-2.852095642E+02 *S101363 *S101363 5 3 3.201828613E+02 *S101364 *S101364 6 3-3.201842957E+02 *S101365 *S101365 7 3 2.406595154E+02 *S101366 *S101366 8 3-2.406607208E+02 *S101367 *S101367 9 3 1.587675476E+02 *S101368 *S101368 10 3-1.587682037E+02 *S101369 *S101369 99 3 1.070013281E+05 *S101370 *S101370 99 5-1.430872656E+05 *S101371 *S101371 99 2-1.967195508E+04 *S101372 *S101372 99 6 7.832183125E+05 *S101373 DMIG *AEROS117 99 2 *S101374 *S101374 1 3 4.973302460E+01 *S101375 *S101375 2 3-4.973326111E+01 *S101376 *S101376 3 3 3.836505508E+01 *S101377 *S101377 4 3-3.921124649E+01 *S101378 *S101378 5 3 4.401945114E+01 *S101379 *S101379 6 3-4.401964951E+01 *S101380 *S101380 7 3 3.308640671E+01 *S101381 *S101381 8 3-3.308657074E+01 *S101382 *S101382 9 3 2.182771492E+01 *S101383 *S101383 10 3-2.182780647E+01 *S101384 *S101384 99 3 8.460307717E-01 *S101385 *S101385 99 5 0.000000000E+00 *S101386 *S101386 99 2 0.000000000E+00 *S101387 *S101387 99 6 0.000000000E+00 *S101388 DMIG *AEROS117 99 6 *S101389 *S101389 1 3-1.980068237E+03 *S101390 *S101390 2 3 1.980077759E+03 *S101391 *S101391 3 3-1.527464600E+03 *S101392 *S101392 4 3 1.561154663E+03 *S101393 *S101393 5 3-1.752588379E+03 *S101394 *S101394 6 3 1.752596313E+03 *S101395 *S101395 7 3-1.317300659E+03 *S101396 *S101396 8 3 1.317307129E+03 *S101397 *S101397 9 3-8.690476074E+02 *S101398 *S101398 10 3 8.690512695E+02 *S101399 *S101399 99 3-1.970563867E+04 *S101400 *S101400 99 5-7.832183125E+05 *S101401 *S101401 99 2-1.069951719E+05 *S101402 *S101402 99 6-1.430872656E+05 *S101403 DMIG AEROB117 0 1 1 DMIG *AEROB117 99 3 *D101408 *D101408 99 3 4.692770958E+00 *D101409 *D101409 99 5-6.275757313E+00 *D101410 *D101410 99 2-8.628050089E-01 *D101411 *D101411 99 6 3.435168076E+01 *D101412 DMIG *AEROB117 99 5 *D101413 *D101413 99 3 0.000000000E+00 *D101414 *D101414 99 5 3.514564514E+02 *D101415 *D101415 99 2 3.435168076E+01 *D101416 *D101416 99 6-5.249324375E+05 *D101417 DMIG *AEROB117 99 2 *D101418 *D101418 99 3 8.628050089E-01 *D101419 *D101419 99 5 3.435168076E+01 *D101420 *D101420 99 2 4.692770958E+00 *D101421 *D101421 99 6 6.275757313E+00 *D101422 DMIG *AEROB117 99 6 *D101423 *D101423 99 3 3.435168076E+01 *D101424 *D101424 99 5 5.249324375E+05 *D101425 *D101425 99 2 0.000000000E+00 *D101426 *D101426 99 6 3.514564514E+02 *D101427 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ 7 FOOT PROP W/WASH - PROP1_2000.DAT - 2000rpm - DEC,1988 - SSOUND=10E6 $ THE FOLLOWING MATRICES (AEROS118 AND AEROB118) ARE BASED ON $ VELOCITY = 2.000000E+03(ft/sec) $ MACH NO = 2.000000E-04 $ DENSITY = 1.146800E-07 DMIG AEROS118 0 1 1 DMIG *AEROS118 99 3 *S101428 *S101428 1 3-3.025823669E+02 *S101429 *S101429 2 3 3.025838318E+02 *S101430 *S101430 3 3-2.334181519E+02 *S101431 *S101431 4 3 2.385664825E+02 *S101432 *S101432 5 3-2.678202515E+02 *S101433 *S101433 6 3 2.678214417E+02 *S101434 *S101434 7 3-2.013021240E+02 *S101435 *S101435 8 3 2.013031311E+02 *S101436 *S101436 9 3-1.328027344E+02 *S101437 *S101437 10 3 1.328032990E+02 *S101438 *S101438 99 3-5.147364616E+00 *S101439 *S101439 99 5 0.000000000E+00 *S101440 *S101440 99 2 0.000000000E+00 *S101441 *S101441 99 6 0.000000000E+00 *S101442 DMIG *AEROS118 99 5