$ $ file prop1.dat - referred to as tnd1807 in the notes $ $ The dmap propa.v2004 is not needed for this run. The features $ are included in SOL 145. $ $ ID PROP, TEST ID PROP, PROP1 $ run 12/23/88 - using results from latest version of PROPT - no WASH $ $ SAMPLE AERO PROBLEM WITH PROP TERMS - NASA D-1807 $ TIME 25 diag 8,49 sol 145 CEND TITLE = PROP WHIRL SAMPLE - PROP FROM NASA D-1807 - data from PROP1 SUBT = User-supplied Aspect ratio - 12/23/88 LABEL = PK METHOD FLUTTER SOLUTION - NO DMIG ON SUB 1 SEALL=ALL SPC = 1 SUBCASE 1 LABEL = SUBCASE 1 - FMETHOD = 30 - VELOCITY = 1 FT/SEC METHOD = 10 FMETHOD = 30 $ B2PP=AEROB101 $ K2PP=AEROS101 SUBCASE 2 LABEL = SUBCASE 2 - FMETHOD = 40 - VELOCITY = 10 FT/SEC METHOD = 10 FMETHOD = 40 B2PP=AEROB102 K2PP=AEROS102 SUBCASE 3 LABEL = SUBCASE 3 - FMETHOD = 50 - VELOCITY = 20 FT/SEC METHOD = 10 FMETHOD = 50 B2PP=AEROB103 K2PP=AEROS103 SUBCASE 4 LABEL = SUBCASE 4 - FMETHOD = 60 - VELOCITY = 30 FT/SEC METHOD = 10 FMETHOD = 60 B2PP=AEROB104 K2PP=AEROS104 SUBCASE 5 LABEL = SUBCASE 5 - FMETHOD = 70 - VELOCITY = 40 FT/SEC METHOD = 10 FMETHOD = 70 B2PP=AEROB105 K2PP=AEROS105 SUBCASE 6 LABEL = SUBCASE 6 - FMETHOD = 80 - VELOCITY = 50 FT/SEC METHOD = 10 FMETHOD = 80 B2PP=AEROB106 K2PP=AEROS106 SUBCASE 7 LABEL = SUBCASE 7 - FMETHOD = 90 - VELOCITY = 60 FT/SEC METHOD = 10 FMETHOD = 90 B2PP=AEROB107 K2PP=AEROS107 SUBCASE 8 LABEL = SUBCASE 8 - FMETHOD = 100 - VELOCITY = 70 FT/SEC METHOD = 10 FMETHOD = 100 B2PP=AEROB108 K2PP=AEROS108 SUBCASE 9 LABEL = SUBCASE 9 - FMETHOD = 110 - VELOCITY = 80 FT/SEC METHOD = 10 FMETHOD = 110 B2PP=AEROB109 K2PP=AEROS109 SUBCASE 10 LABEL = SUBCASE 10 - FMETHOD = 120 - VELOCITY = 90 FT/SEC METHOD = 10 FMETHOD = 120 B2PP=AEROB110 K2PP=AEROS110 SUBCASE 11 LABEL = SUBCASE 11 - FMETHOD = 130 - VELOCITY = 100 FT/SEC METHOD = 10 FMETHOD = 130 B2PP=AEROB111 K2PP=AEROS111 SUBCASE 12 LABEL = SUBCASE 12 - FMETHOD = 140 - VELOCITY = 110 FT/SEC METHOD = 10 FMETHOD = 140 B2PP=AEROB112 K2PP=AEROS112 $ BEGIN BULK $ $ PROP GRID IS 999 - ATTACHED TO GRID 1000 BY CELAS FOR FREQUENCIES $ GRID 999 .0 0.000 .0 15 RBAR 1000 999 1000 123456 GRID 1000 3.5035 0.0 .0 1234 $ coordinate system for prop points - pointing -x and -z CORD2R 15 0. 0. 0. 0. 0. -1. +cr15 +cr15 -1. 0. 0. $ $ CONCENTRATED MASS FOR PROP $ CONM2 999 999 3.82711 +PROP +PROP 246.761 246.761 $ PARAM WTMASS .0025901 $ $ CELAS2 ELEMENTS TO OBTAIN FREQUENCIES $ CELAS2 1 2542.2 1000 5 CELAS2 2 2498.2 1000 6 EIGR 10 GIV .0 30. 3 +ER +ER MAX $ SET DENSITY FLFACT 1 0.8873 DENS FLFACT 2 0.10 MACH $ ONE VELOCITY PER SUBCASE FLFACT 3 1.0 VELOC FLFACT 4 120. VELOC FLFACT 5 240. VELOC FLFACT 6 360. VELOC FLFACT 7 480. VELOC FLFACT 8 600. VELOC FLFACT 9 720. VELOC FLFACT 10 840. VELOC FLFACT 11 -960. VELOC FLFACT 12 -1080. VELOC FLFACT 13 1200. VELOC FLFACT 14 1320. VELOC $ set up flutter cases FLUTTER 30 PK 1 2 3 L 2 FLUTTER 40 PK 1 2 4 L 2 FLUTTER 50 PK 1 2 5 L 2 FLUTTER 60 PK 1 2 6 L 2 FLUTTER 70 PK 1 2 7 L 2 FLUTTER 80 PK 1 2 8 L 2 FLUTTER 90 PK 1 2 9 L 2 FLUTTER 100 PK 1 2 10 L 2 FLUTTER 110 PK 1 2 11 L 2 FLUTTER 120 PK 1 2 12 L 2 FLUTTER 130 PK 1 2 13 L 2 FLUTTER 140 PK 1 2 14 L 2 PARAM LMODES 3 PARAM VREF 12.0 $ $ AERO CARD FOR REF CHORD = 4.375 $ AERO 4.375 1.1468-7 $ CAERO1 2000 2000 2 2 1 +CAC +CAC 0. 0. 0. 1.0 0. 1.0 0. 1.0 PAERO1 2000 MKAERO1 0.0 +MK +MK .001 GRID 1001 0.0 0.0 0.0 123456 GRID 1002 1.0 0.0 0.0 123456 GRID 1003 0.0 1.0 0.0 12456 CELAS2 1004 1.0+6 1003 3 CONM2 1004 1003 1.0 SPLINE2 2000 2000 2000 2003 2000 0. 1. +SPC +SPC -1. -1. SET1 2000 1001 1002 1003 $ $ damping elements $ CDAMP1,101,101,999,5 CDAMP1,102,102,999,6 PDAMP,101,.26387,102,.39237 $ $ DMIG cards created by PROP using input from D1807A.DAT $ $ $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS101 AND AEROB101) ARE BASED ON $ VELOCITY = 1.000000E-01(ft/sec) $ MACH NO = 8.960574E-05 $ DENSITY = 1.017600E-07 DMIG AEROS101 0 1 1 DMIG *AEROS101 999 3 *S100001 *S100001 999 3 0.000000000E+00 *S100002 *S100002 999 5 0.000000000E+00 *S100003 *S100003 999 2 0.000000000E+00 *S100004 *S100004 999 6 0.000000000E+00 *S100005 DMIG *AEROS101 999 5 *S100006 *S100006 999 3 1.234218416E-08 *S100007 *S100007 999 5-2.162004057E-05 *S100008 *S100008 999 2-3.099551948E-09 *S100009 *S100009 999 6 8.248916129E-05 *S100010 DMIG *AEROS101 999 2 *S100011 *S100011 999 3 0.000000000E+00 *S100012 *S100012 999 5 0.000000000E+00 *S100013 *S100013 999 2 0.000000000E+00 *S100014 *S100014 999 6 0.000000000E+00 *S100015 DMIG *AEROS101 999 6 *S100016 *S100016 999 3-3.099551948E-09 *S100017 *S100017 999 5-8.248916129E-05 *S100018 *S100018 999 2-1.234218416E-08 *S100019 *S100019 999 6-2.162004057E-05 *S100020 DMIG AEROB101 0 1 1 DMIG *AEROB101 999 3 *D100021 *D100021 999 3 1.028515317E-08 *D100022 *D100022 999 5-1.801669896E-05 *D100023 *D100023 999 2-2.582960068E-09 *D100024 *D100024 999 6 6.874097016E-05 *D100025 DMIG *AEROB101 999 5 *D100026 *D100026 999 3 0.000000000E+00 *D100027 *D100027 999 5 7.760576010E-01 *D100028 *D100028 999 2 6.874097016E-05 *D100029 *D100029 999 6-2.484055328E+01 *D100030 DMIG *AEROB101 999 2 *D100031 *D100031 999 3 2.582960068E-09 *D100032 *D100032 999 5 6.874097016E-05 *D100033 *D100033 999 2 1.028515317E-08 *D100034 *D100034 999 6 1.801669896E-05 *D100035 DMIG *AEROB101 999 6 *D100036 *D100036 999 3 6.874097016E-05 *D100037 *D100037 999 5 2.484055328E+01 *D100038 *D100038 999 2 0.000000000E+00 *D100039 *D100039 999 6 7.760576010E-01 *D100040 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS102 AND AEROB102) ARE BASED ON $ VELOCITY = 1.000000E+01(ft/sec) $ MACH NO = 8.960574E-03 $ DENSITY = 1.017600E-07 DMIG AEROS102 0 1 1 DMIG *AEROS102 999 3 *S100042 *S100042 999 3 0.000000000E+00 *S100043 *S100043 999 5 0.000000000E+00 *S100044 *S100044 999 2 0.000000000E+00 *S100045 *S100045 999 6 0.000000000E+00 *S100046 DMIG *AEROS102 999 5 *S100047 *S100047 999 3 1.225770824E-02 *S100048 *S100048 999 5-2.157183588E-01 *S100049 *S100049 999 2-3.085949691E-03 *S100050 *S100050 999 6 8.224641085E-01 *S100051 DMIG *AEROS102 999 2 *S100052 *S100052 999 3 0.000000000E+00 *S100053 *S100053 999 5 0.000000000E+00 *S100054 *S100054 999 2 0.000000000E+00 *S100055 *S100055 999 6 0.000000000E+00 *S100056 DMIG *AEROS102 999 6 *S100057 *S100057 999 3-3.085949691E-03 *S100058 *S100058 999 5-8.224641085E-01 *S100059 *S100059 999 2-1.225770824E-02 *S100060 *S100060 999 6-2.157183588E-01 *S100061 DMIG AEROB102 0 1 1 DMIG *AEROB102 999 3 *D100062 *D100062 999 3 1.021475618E-04 *D100063 *D100063 999 5-1.797652920E-03 *D100064 *D100064 999 2-2.571624645E-05 *D100065 *D100065 999 6 6.853867322E-03 *D100066 DMIG *AEROB102 999 5 *D100067 *D100067 999 3 0.000000000E+00 *D100068 *D100068 999 5 7.747367620E-01 *D100069 *D100069 999 2 6.853867788E-03 *D100070 *D100070 999 6-2.484055328E+01 *D100071 DMIG *AEROB102 999 2 *D100072 *D100072 999 3 2.571624645E-05 *D100073 *D100073 999 5 6.853867322E-03 *D100074 *D100074 999 2 1.021475618E-04 *D100075 *D100075 999 6 1.797652920E-03 *D100076 DMIG *AEROB102 999 6 *D100077 *D100077 999 3 6.853867788E-03 *D100078 *D100078 999 5 2.484055328E+01 *D100079 *D100079 999 2 0.000000000E+00 *D100080 *D100080 999 6 7.747367620E-01 *D100081 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS103 AND AEROB103) ARE BASED ON $ VELOCITY = 2.000000E+01(ft/sec) $ MACH NO = 1.792115E-02 $ DENSITY = 1.017600E-07 DMIG AEROS103 0 1 1 DMIG *AEROS103 999 3 *S100083 *S100083 999 3 0.000000000E+00 *S100084 *S100084 999 5 0.000000000E+00 *S100085 *S100085 999 2 0.000000000E+00 *S100086 *S100086 999 6 0.000000000E+00 *S100087 DMIG *AEROS103 999 5 *S100088 *S100088 999 3 9.620226175E-02 *S100089 *S100089 999 5-8.572272062E-01 *S100090 *S100090 999 2-2.437965386E-02 *S100091 *S100091 999 6 3.262063980E+00 *S100092 DMIG *AEROS103 999 2 *S100093 *S100093 999 3 0.000000000E+00 *S100094 *S100094 999 5 0.000000000E+00 *S100095 *S100095 999 2 0.000000000E+00 *S100096 *S100096 999 6 0.000000000E+00 *S100097 DMIG *AEROS103 999 6 *S100098 *S100098 999 3-2.437965386E-02 *S100099 *S100099 999 5-3.262063980E+00 *S100100 *S100100 999 2-9.620226175E-02 *S100101 *S100101 999 6-8.572272062E-01 *S100102 DMIG AEROB103 0 1 1 DMIG *AEROB103 999 3 *D100103 *D100103 999 3 4.008427204E-04 *D100104 *D100104 999 5-3.571780166E-03 *D100105 *D100105 999 2-1.015818852E-04 *D100106 *D100106 999 6 1.359193306E-02 *D100107 DMIG *AEROB103 999 5 *D100108 *D100108 999 3 0.000000000E+00 *D100109 *D100109 999 5 7.708566785E-01 *D100110 *D100110 999 2 1.359193400E-02 *D100111 *D100111 999 6-2.484055328E+01 *D100112 DMIG *AEROB103 999 2 *D100113 *D100113 999 3 1.015818852E-04 *D100114 *D100114 999 5 1.359193306E-02 *D100115 *D100115 999 2 4.008427204E-04 *D100116 *D100116 999 6 3.571780166E-03 *D100117 DMIG *AEROB103 999 6 *D100118 *D100118 999 3 1.359193400E-02 *D100119 *D100119 999 5 2.484055328E+01 *D100120 *D100120 999 2 0.000000000E+00 *D100121 *D100121 999 6 7.708566785E-01 *D100122 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS104 AND AEROB104) ARE BASED ON $ VELOCITY = 3.000000E+01(ft/sec) $ MACH NO = 2.688172E-02 $ DENSITY = 1.017600E-07 DMIG AEROS104 0 1 1 DMIG *AEROS104 999 3 *S100124 *S100124 999 3 0.000000000E+00 *S100125 *S100125 999 5 0.000000000E+00 *S100126 *S100126 999 2 0.000000000E+00 *S100127 *S100127 999 6 0.000000000E+00 *S100128 DMIG *AEROS104 999 5 *S100129 *S100129 999 3 3.156787753E-01 *S100130 *S100130 999 5-1.908492208E+00 *S100131 *S100131 999 2-8.071389049E-02 *S100132 *S100132 999 6 7.243706703E+00 *S100133 DMIG *AEROS104 999 2 *S100134 *S100134 999 3 0.000000000E+00 *S100135 *S100135 999 5 0.000000000E+00 *S100136 *S100136 999 2 0.000000000E+00 *S100137 *S100137 999 6 0.000000000E+00 *S100138 DMIG *AEROS104 999 6 *S100139 *S100139 999 3-8.071389049E-02 *S100140 *S100140 999 5-7.243706703E+00 *S100141 *S100141 999 2-3.156787753E-01 *S100142 *S100142 999 6-1.908492208E+00 *S100143 DMIG AEROB104 0 1 1 DMIG *AEROB104 999 3 *D100144 *D100144 999 3 8.768855478E-04 *D100145 *D100145 999 5-5.301367026E-03 *D100146 *D100146 999 2-2.242052724E-04 *D100147 *D100147 999 6 2.012140863E-02 *D100148 DMIG *AEROB104 999 5 *D100149 *D100149 999 3 0.000000000E+00 *D100150 *D100150 999 5 7.646378875E-01 *D100151 *D100151 999 2 2.012140676E-02 *D100152 *D100152 999 6-2.484055328E+01 *D100153 DMIG *AEROB104 999 2 *D100154 *D100154 999 3 2.242052724E-04 *D100155 *D100155 999 5 2.012140863E-02 *D100156 *D100156 999 2 8.768855478E-04 *D100157 *D100157 999 6 5.301367026E-03 *D100158 DMIG *AEROB104 999 6 *D100159 *D100159 999 3 2.012140676E-02 *D100160 *D100160 999 5 2.484055328E+01 *D100161 *D100161 999 2 0.000000000E+00 *D100162 *D100162 999 6 7.646378875E-01 *D100163 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS105 AND AEROB105) ARE BASED ON $ VELOCITY = 4.000000E+01(ft/sec) $ MACH NO = 3.584230E-02 $ DENSITY = 1.017600E-07 DMIG AEROS105 0 1 1 DMIG *AEROS105 999 3 *S100165 *S100165 999 3 0.000000000E+00 *S100166 *S100166 999 5 0.000000000E+00 *S100167 *S100167 999 2 0.000000000E+00 *S100168 *S100168 999 6 0.000000000E+00 *S100169 DMIG *AEROS105 999 5 *S100170 *S100170 999 3 7.234327197E-01 *S100171 *S100171 999 5-3.345230341E+00 *S100172 *S100172 999 2-1.867179573E-01 *S100173 *S100173 999 6 1.266260338E+01 *S100174 DMIG *AEROS105 999 2 *S100175 *S100175 999 3 0.000000000E+00 *S100176 *S100176 999 5 0.000000000E+00 *S100177 *S100177 999 2 0.000000000E+00 *S100178 *S100178 999 6 0.000000000E+00 *S100179 DMIG *AEROS105 999 6 *S100180 *S100180 999 3-1.867179573E-01 *S100181 *S100181 999 5-1.266260338E+01 *S100182 *S100182 999 2-7.234327197E-01 *S100183 *S100183 999 6-3.345230341E+00 *S100184 DMIG AEROB105 0 1 1 DMIG *AEROB105 999 3 *D100185 *D100185 999 3 1.507151523E-03 *D100186 *D100186 999 5-6.969229784E-03 *D100187 *D100187 999 2-3.889957443E-04 *D100188 *D100188 999 6 2.638042346E-02 *D100189 DMIG *AEROB105 999 5 *D100190 *D100190 999 3 0.000000000E+00 *D100191 *D100191 999 5 7.563803792E-01 *D100192 *D100192 999 2 2.638042346E-02 *D100193 *D100193 999 6-2.484055328E+01 *D100194 DMIG *AEROB105 999 2 *D100195 *D100195 999 3 3.889957443E-04 *D100196 *D100196 999 5 2.638042346E-02 *D100197 *D100197 999 2 1.507151523E-03 *D100198 *D100198 999 6 6.969229784E-03 *D100199 DMIG *AEROB105 999 6 *D100200 *D100200 999 3 2.638042346E-02 *D100201 *D100201 999 5 2.484055328E+01 *D100202 *D100202 999 2 0.000000000E+00 *D100203 *D100203 999 6 7.563803792E-01 *D100204 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS106 AND AEROB106) ARE BASED ON $ VELOCITY = 5.000000E+01(ft/sec) $ MACH NO = 4.480287E-02 $ DENSITY = 1.017600E-07 DMIG AEROS106 0 1 1 DMIG *AEROS106 999 3 *S100206 *S100206 999 3 0.000000000E+00 *S100207 *S100207 999 5 0.000000000E+00 *S100208 *S100208 999 2 0.000000000E+00 *S100209 *S100209 999 6 0.000000000E+00 *S100210 DMIG *AEROS106 999 5 *S100211 *S100211 999 3 1.361783147E+00 *S100212 *S100212 999 5-5.137341499E+00 *S100213 *S100213 999 2-3.545427620E-01 *S100214 *S100214 999 6 1.940024567E+01 *S100215 DMIG *AEROS106 999 2 *S100216 *S100216 999 3 0.000000000E+00 *S100217 *S100217 999 5 0.000000000E+00 *S100218 *S100218 999 2 0.000000000E+00 *S100219 *S100219 999 6 0.000000000E+00 *S100220 DMIG *AEROS106 999 6 *S100221 *S100221 999 3-3.545427620E-01 *S100222 *S100222 999 5-1.940024567E+01 *S100223 *S100223 999 2-1.361783147E+00 *S100224 *S100224 999 6-5.137341499E+00 *S100225 DMIG AEROB106 0 1 1 DMIG *AEROB106 999 3 *D100226 *D100226 999 3 2.269638702E-03 *D100227 *D100227 999 5-8.562236093E-03 *D100228 *D100228 999 2-5.909046158E-04 *D100229 *D100229 999 6 3.233374283E-02 *D100230 DMIG *AEROB106 999 5 *D100231 *D100231 999 3 0.000000000E+00 *D100232 *D100232 999 5 7.464115620E-01 *D100233 *D100233 999 2 3.233374283E-02 *D100234 *D100234 999 6-2.484055328E+01 *D100235 DMIG *AEROB106 999 2 *D100236 *D100236 999 3 5.909046158E-04 *D100237 *D100237 999 5 3.233374283E-02 *D100238 *D100238 999 2 2.269638702E-03 *D100239 *D100239 999 6 8.562236093E-03 *D100240 DMIG *AEROB106 999 6 *D100241 *D100241 999 3 3.233374283E-02 *D100242 *D100242 999 5 2.484055328E+01 *D100243 *D100243 999 2 0.000000000E+00 *D100244 *D100244 999 6 7.464115620E-01 *D100245 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS107 AND AEROB107) ARE BASED ON $ VELOCITY = 6.000000E+01(ft/sec) $ MACH NO = 5.376344E-02 $ DENSITY = 1.017600E-07 DMIG AEROS107 0 1 1 DMIG *AEROS107 999 3 *S100247 *S100247 999 3 0.000000000E+00 *S100248 *S100248 999 5 0.000000000E+00 *S100249 *S100249 999 2 0.000000000E+00 *S100250 *S100250 999 6 0.000000000E+00 *S100251 DMIG *AEROS107 999 5 *S100252 *S100252 999 3 2.264612436E+00 *S100253 *S100253 999 5-7.251149178E+00 *S100254 *S100254 999 2-5.939050317E-01 *S100255 *S100255 999 6 2.733502769E+01 *S100256 DMIG *AEROS107 999 2 *S100257 *S100257 999 3 0.000000000E+00 *S100258 *S100258 999 5 0.000000000E+00 *S100259 *S100259 999 2 0.000000000E+00 *S100260 *S100260 999 6 0.000000000E+00 *S100261 DMIG *AEROS107 999 6 *S100262 *S100262 999 3-5.939050317E-01 *S100263 *S100263 999 5-2.733502769E+01 *S100264 *S100264 999 2-2.264612436E+00 *S100265 *S100265 999 6-7.251149178E+00 *S100266 DMIG AEROB107 0 1 1 DMIG *AEROB107 999 3 *D100267 *D100267 999 3 3.145295428E-03 *D100268 *D100268 999 5-1.007104106E-02 *D100269 *D100269 999 2-8.248680970E-04 *D100270 *D100270 999 6 3.796531633E-02 *D100271 DMIG *AEROB107 999 5 *D100272 *D100272 999 3 0.000000000E+00 *D100273 *D100273 999 5 7.350545526E-01 *D100274 *D100274 999 2 3.796531633E-02 *D100275 *D100275 999 6-2.484055328E+01 *D100276 DMIG *AEROB107 999 2 *D100277 *D100277 999 3 8.248680970E-04 *D100278 *D100278 999 5 3.796531633E-02 *D100279 *D100279 999 2 3.145295428E-03 *D100280 *D100280 999 6 1.007104106E-02 *D100281 DMIG *AEROB107 999 6 *D100282 *D100282 999 3 3.796531633E-02 *D100283 *D100283 999 5 2.484055328E+01 *D100284 *D100284 999 2 0.000000000E+00 *D100285 *D100285 999 6 7.350545526E-01 *D100286 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS108 AND AEROB108) ARE BASED ON $ VELOCITY = 7.000000E+01(ft/sec) $ MACH NO = 6.272402E-02 $ DENSITY = 1.017600E-07 DMIG AEROS108 0 1 1 DMIG *AEROS108 999 3 *S100288 *S100288 999 3 0.000000000E+00 *S100289 *S100289 999 5 0.000000000E+00 *S100290 *S100290 999 2 0.000000000E+00 *S100291 *S100291 999 6 0.000000000E+00 *S100292 DMIG *AEROS108 999 5 *S100293 *S100293 999 3 3.459257126E+00 *S100294 *S100294 999 5-9.651294708E+00 *S100295 *S100295 999 2-9.122828245E-01 *S100296 *S100296 999 6 3.634852982E+01 *S100297 DMIG *AEROS108 999 2 *S100298 *S100298 999 3 0.000000000E+00 *S100299 *S100299 999 5 0.000000000E+00 *S100300 *S100300 999 2 0.000000000E+00 *S100301 *S100301 999 6 0.000000000E+00 *S100302 DMIG *AEROS108 999 6 *S100303 *S100303 999 3-9.122828245E-01 *S100304 *S100304 999 5-3.634852982E+01 *S100305 *S100305 999 2-3.459257126E+00 *S100306 *S100306 999 6-9.651294708E+00 *S100307 DMIG AEROB108 0 1 1 DMIG *AEROB108 999 3 *D100308 *D100308 999 3 4.118163604E-03 *D100309 *D100309 999 5-1.148963906E-02 *D100310 *D100310 999 2-1.086051110E-03 *D100311 *D100311 999 6 4.327207059E-02 *D100312 DMIG *AEROB108 999 5 *D100313 *D100313 999 3 0.000000000E+00 *D100314 *D100314 999 5 7.226121426E-01 *D100315 *D100315 999 2 4.327206686E-02 *D100316 *D100316 999 6-2.484055328E+01 *D100317 DMIG *AEROB108 999 2 *D100318 *D100318 999 3 1.086051110E-03 *D100319 *D100319 999 5 4.327207059E-02 *D100320 *D100320 999 2 4.118163604E-03 *D100321 *D100321 999 6 1.148963906E-02 *D100322 DMIG *AEROB108 999 6 *D100323 *D100323 999 3 4.327206686E-02 *D100324 *D100324 999 5 2.484055328E+01 *D100325 *D100325 999 2 0.000000000E+00 *D100326 *D100326 999 6 7.226121426E-01 *D100327 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS109 AND AEROB109) ARE BASED ON $ VELOCITY = 8.000000E+01(ft/sec) $ MACH NO = 7.168459E-02 $ DENSITY = 1.017600E-07 DMIG AEROS109 0 1 1 DMIG *AEROS109 999 3 *S100329 *S100329 999 3 0.000000000E+00 *S100330 *S100330 999 5 0.000000000E+00 *S100331 *S100331 999 2 0.000000000E+00 *S100332 *S100332 999 6 0.000000000E+00 *S100333 DMIG *AEROS109 999 5 *S100334 *S100334 999 3 4.967974186E+00 *S100335 *S100335 999 5-1.230223751E+01 *S100336 *S100336 999 2-1.315175176E+00 *S100337 *S100337 999 6 4.632906723E+01 *S100338 DMIG *AEROS109 999 2 *S100339 *S100339 999 3 0.000000000E+00 *S100340 *S100340 999 5 0.000000000E+00 *S100341 *S100341 999 2 0.000000000E+00 *S100342 *S100342 999 6 0.000000000E+00 *S100343 DMIG *AEROS109 999 6 *S100344 *S100344 999 3-1.315175176E+00 *S100345 *S100345 999 5-4.632906723E+01 *S100346 *S100346 999 2-4.967974186E+00 *S100347 *S100347 999 6-1.230223751E+01 *S100348 DMIG AEROB109 0 1 1 DMIG *AEROB109 999 3 *D100349 *D100349 999 3 5.174973048E-03 *D100350 *D100350 999 5-1.281483006E-02 *D100351 *D100351 999 2-1.369974110E-03 *D100352 *D100352 999 6 4.825944826E-02 *D100353 DMIG *AEROB109 999 5 *D100354 *D100354 999 3 0.000000000E+00 *D100355 *D100355 999 5 7.093558311E-01 *D100356 *D100356 999 2 4.825944826E-02 *D100357 *D100357 999 6-2.484055328E+01 *D100358 DMIG *AEROB109 999 2 *D100359 *D100359 999 3 1.369974110E-03 *D100360 *D100360 999 5 4.825944826E-02 *D100361 *D100361 999 2 5.174973048E-03 *D100362 *D100362 999 6 1.281483006E-02 *D100363 DMIG *AEROB109 999 6 *D100364 *D100364 999 3 4.825944826E-02 *D100365 *D100365 999 5 2.484055328E+01 *D100366 *D100366 999 2 0.000000000E+00 *D100367 *D100367 999 6 7.093558311E-01 *D100368 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS110 AND AEROB110) ARE BASED ON $ VELOCITY = 9.000000E+01(ft/sec) $ MACH NO = 8.064516E-02 $ DENSITY = 1.017600E-07 DMIG AEROS110 0 1 1 DMIG *AEROS110 999 3 *S100370 *S100370 999 3 0.000000000E+00 *S100371 *S100371 999 5 0.000000000E+00 *S100372 *S100372 999 2 0.000000000E+00 *S100373 *S100373 999 6 0.000000000E+00 *S100374 DMIG *AEROS110 999 5 *S100375 *S100375 999 3 6.809050560E+00 *S100376 *S100376 999 5-1.516941452E+01 *S100377 *S100377 999 2-1.806382418E+00 *S100378 *S100378 999 6 5.717358398E+01 *S100379 DMIG *AEROS110 999 2 *S100380 *S100380 999 3 0.000000000E+00 *S100381 *S100381 999 5 0.000000000E+00 *S100382 *S100382 999 2 0.000000000E+00 *S100383 *S100383 999 6 0.000000000E+00 *S100384 DMIG *AEROS110 999 6 *S100385 *S100385 999 3-1.806382418E+00 *S100386 *S100386 999 5-5.717358398E+01 *S100387 *S100387 999 2-6.809050560E+00 *S100388 *S100388 999 6-1.516941452E+01 *S100389 DMIG AEROB110 0 1 1 DMIG *AEROB110 999 3 *D100390 *D100390 999 3 6.304676179E-03 *D100391 *D100391 999 5-1.404575445E-02 *D100392 *D100392 999 2-1.672576298E-03 *D100393 *D100393 999 6 5.293850228E-02 *D100394 DMIG *AEROB110 999 5 *D100395 *D100395 999 3 0.000000000E+00 *D100396 *D100396 999 5 6.955250502E-01 *D100397 *D100397 999 2 5.293850228E-02 *D100398 *D100398 999 6-2.484055328E+01 *D100399 DMIG *AEROB110 999 2 *D100400 *D100400 999 3 1.672576298E-03 *D100401 *D100401 999 5 5.293850228E-02 *D100402 *D100402 999 2 6.304676179E-03 *D100403 *D100403 999 6 1.404575445E-02 *D100404 DMIG *AEROB110 999 6 *D100405 *D100405 999 3 5.293850228E-02 *D100406 *D100406 999 5 2.484055328E+01 *D100407 *D100407 999 2 0.000000000E+00 *D100408 *D100408 999 6 6.955250502E-01 *D100409 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS111 AND AEROB111) ARE BASED ON $ VELOCITY = 1.000000E+02(ft/sec) $ MACH NO = 8.960573E-02 $ DENSITY = 1.017600E-07 DMIG AEROS111 0 1 1 DMIG *AEROS111 999 3 *S100411 *S100411 999 3 0.000000000E+00 *S100412 *S100412 999 5 0.000000000E+00 *S100413 *S100413 999 2 0.000000000E+00 *S100414 *S100414 999 6 0.000000000E+00 *S100415 DMIG *AEROS111 999 5 *S100416 *S100416 999 3 8.997632980E+00 *S100417 *S100417 999 5-1.822004890E+01 *S100418 *S100418 999 2-2.388283014E+00 *S100419 *S100419 999 6 6.878847504E+01 *S100420 DMIG *AEROS111 999 2 *S100421 *S100421 999 3 0.000000000E+00 *S100422 *S100422 999 5 0.000000000E+00 *S100423 *S100423 999 2 0.000000000E+00 *S100424 *S100424 999 6 0.000000000E+00 *S100425 DMIG *AEROS111 999 6 *S100426 *S100426 999 3-2.388283014E+00 *S100427 *S100427 999 5-6.878847504E+01 *S100428 *S100428 999 2-8.997632980E+00 *S100429 *S100429 999 6-1.822004890E+01 *S100430 DMIG AEROB111 0 1 1 DMIG *AEROB111 999 3 *D100431 *D100431 999 3 7.498027291E-03 *D100432 *D100432 999 5-1.518337522E-02 *D100433 *D100433 999 2-1.990235876E-03 *D100434 *D100434 999 6 5.732372776E-02 *D100435 DMIG *AEROB111 999 5 *D100436 *D100436 999 3 0.000000000E+00 *D100437 *D100437 999 5 6.813251376E-01 *D100438 *D100438 999 2 5.732373148E-02 *D100439 *D100439 999 6-2.484055328E+01 *D100440 DMIG *AEROB111 999 2 *D100441 *D100441 999 3 1.990235876E-03 *D100442 *D100442 999 5 5.732372776E-02 *D100443 *D100443 999 2 7.498027291E-03 *D100444 *D100444 999 6 1.518337522E-02 *D100445 DMIG *AEROB111 999 6 *D100446 *D100446 999 3 5.732373148E-02 *D100447 *D100447 999 5 2.484055328E+01 *D100448 *D100448 999 2 0.000000000E+00 *D100449 *D100449 999 6 6.813251376E-01 *D100450 $ RESULTS FROM PROGRAM PROP FOR THE FOLLOWING PROBLEM $ D-1807 - run 1 - omega=2304 - A=3.47 $ THE FOLLOWING MATRICES (AEROS112 AND AEROB112) ARE BASED ON $ VELOCITY = 1.100000E+02(ft/sec) $ MACH NO = 9.856631E-02 $ DENSITY = 1.017600E-07 DMIG AEROS112 0 1 1 DMIG *AEROS112 999 3 *S100452 *S100452 999 3 0.000000000E+00 *S100453 *S100453 999 5 0.000000000E+00 *S100454 *S100454 999 2 0.000000000E+00 *S100455 *S100455 999 6 0.000000000E+00 *S100456 DMIG *AEROS112 999 5 *S100457 *S100457 999 3 1.154638577E+01 *S100458 *S100458 999 5-2.142366028E+01 *S100459 *S100459 999 2-3.062086821E+00 *S100460 *S100460 999 6 8.108979034E+01 *S100461 DMIG *AEROS112 999 2 *S100462 *S100462 999 3 0.000000000E+00 *S100463 *S100463 999 5 0.000000000E+00 *S100464 *S100464 999 2 0.000000000E+00 *S100465 *S100465 999 6 0.000000000E+00 *S100466 DMIG *AEROS112 999 6 *S100467 *S100467 999 3-3.062086821E+00 *S100468 *S100468 999 5-8.108979034E+01 *S100469 *S100469 999 2-1.154638577E+01 *S100470 *S100470 999 6-2.142366028E+01 *S100471 DMIG AEROB112 0 1 1 DMIG *AEROB112 999 3 *D100472 *D100472 999 3 8.747261949E-03 *D100473 *D100473 999 5-1.623004675E-02 *D100474 *D100474 999 2-2.319762949E-03 *D100475 *D100475 999 6 6.143165752E-02 *D100476 DMIG *AEROB112 999 5 *D100477 *D100477 999 3 0.000000000E+00 *D100478 *D100478 999 5 6.669288278E-01 *D100479 *D100479 999 2 6.143166125E-02 *D100480 *D100480 999 6-2.484055328E+01 *D100481 DMIG *AEROB112 999 2 *D100482 *D100482 999 3 2.319762949E-03 *D100483 *D100483 999 5 6.143165752E-02 *D100484 *D100484 999 2 8.747261949E-03 *D100485 *D100485 999 6 1.623004675E-02 *D100486 DMIG *AEROB112 999 6 *D100487 *D100487 999 3 6.143166125E-02 *D100488 *D100488 999 5 2.484055328E+01 *D100489 *D100489 999 2 0.000000000E+00 *D100490 *D100490 999 6 6.669288278E-01 *D100491 ENDDATA