170
DEPARTMWENT OF OCEAN ENGINEERING AMSSAC MASS~ OF TECHNOLOG Rl Tov , OF' O F-P XO PAESUS, NZ DISTORIO D/A c o NG o~ L qF' LAM E MA2 I LD by 0213 LryLee aa Course XII.IA 00
DEPARTMWENT OF OCEAN ENGINEERINGAMSSAC MASS~ OF TECHNOLOG
Rl Tov , OF' O F-P
XOPAESUS, NZ DISTORIO
D/A
c o NG o~ L qF' LAM E MA2 I LD
by
0213LryLee aa
Course XII.IA
00
-74-
REMOVAL OF OUT-OF-PLANE DISTORTION IN MILD STEEL PANELS
USING FLAME HEATING D TICIELECTE
by 0 E 2 1 8Larry Lee Janca H
B.S., University of California(1976)
SUBMITTED TO THE DEPARTMENT OF OCEAN ENGINEERINGIN PARTIAL FULFILLMENT OF THE REQUIREMENTS
FOR THE DEGREE OF
S.M., NAVAL ARCHITECTURE AND MARINE ENGINEERING
at the
MASSACHUSETTS INSTITUTE OF TECHNOLOGY
May 1987
Copyright @ 1987 Massachusetts Institute of Technology
Signature of Author 2OL JQI Uepartment 0 cean Engineering
May 8, 1987
Certifited by ,i'#< "- - -Koichi Masubuchip a,
Professor,Ocean Engineering and Materials Science7Thesis Supervisor 'a o
Accepted by on
Prof essd=F--Do as CarmichaelChairman, Departmental Graduate Committee---,
Department of Ocean Engineeringion/
AvailabilitY CodeAvail and/or
Drist Sp.o.ilApwoe /c /u~ 6O
APPENDIX F
1/8" STIFFENED PLATE OUT-OF-PLANE DEFLECTION READINGSRECORDED AFTER LINE HEATING THE FIRST PASS
Appendix F contains 10 sets of out-of-plane deflectionmeasurements. The Ist set was recorded after welding butprior to any line heating. The rest were taken after eachpanel was line heated the first time. See Table 2-2 for the1st pass line heating sequence.
NOTE: In appendixes D, E, F, and G the TRANSVERSE andLONGITUDE spacing is 2 inches. All deflection readings in thematrixes are in .001 inches. For example, the out-of-planedistortion at 10 inches TRANSVERSE and 2 inches LONGITUDE, inthe matrix labeled "DISTORTION MEASUREMENTS OF 3/16" PLATEAFTER WELDING" is -0.075 inches (i.e. 0.075 below thereference point). This point is designated D(6,2) as it ison the 6th line in the TRANSVERSE direction and the 2nd linein the LONGITUDE direction.
16h
i DISTORTION MEASUREMENTS OF 1/8" PLATE AFTER WELDING
TRANSVERSE
0 2 4 6 8 10 12 14 16 IS 20 22 24 26 28 30 32 34 36
0:-131 -119 -125 -119 -108 -110 -111 -107 -95 -107 -109 -110 -1232 -130 -84 -104!4 i-101 -146 -74 -58 -49 -89 -736 -153 -46 -67
S8 -94 -144 -45 -42 -16 -49 -3210 -128 -32 -38
112 -80 -109 -124 -120 -97 -60 -21 -15 -14 -13 -9 -1 10 -10 -20 -24 -19 -12 7
14 -114 1 -8
16 -70 -106 4 15 34 -1 40'.18 -96 367
20 1-67-85 5 5 53 1 6
'22 :-57 58 69124 -65. -35 -18 2 28 45 57 68 so 87 93 104 105126 :-60 44 74
L 128 1-65 -88 37 32 99 69 1140 :30 :-88 12 71N 132 -69 -76 36 -3 95 70 129G 34 -63 -3 771 36 1-75 -76 -71 -53 -27 5 38 16 1 0 24 63 102 93 90 91 101 115 134T 38 1-43 7 960 40 :-85 -45 32 19 102 91 135D 42 1-59 33 91E :44 -101 -71 27 35 102 96 133
146 -69 28 9748 -121 -77 -59 -39 6 20 34 46 89 107 113 119 14250 -108 40 9752 -139 -145 -9 38 80 78 121154 -167 24 5556 -166 -186 -35 11 80 39 11158 1-204 -5 3360 -195 -214 -224 -215 -184 -133 -65 -58 -46 -29 -10 12 41 22 16 19 37 63 9662 -222 -44 3
164 -227 -239 -96 -50 IS -3 7966 -253 -57 -2
68 -265 -253 -131 -73 -5 -5 5770 -245 -88 -772 1-301 -259 -234 -212 -169 -126 -109 -87. -45 -18 -1 13 33
USM r V l r1 R. rw '-A ---d a IFR A Vwtwvw
DISTORTION MEASUREMENTS OF 1/8" PLATE AFTER PANEL 5 WAS LINE FLAME HEATED FOR THE FIRST TIME
TRANSVERSE----------------------------------------------------------------------------------------------
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36----------------------------------------------------------------------------------------------
0 -161 -150 -154 -150 -139 -140 -141 -137 -126 -137 -140 -139 -152
2 -162 -115 -135
4 -142 -179 -108 -91 -82 -121 -105
6 -188 -80 -100
8 -126 -180 -82 -76 -50 -83. -66
10 -168 -67 -73
12 -114 -144 -162 -162 -139 -99 -59 -51 -49 -47 -43 -36 -27 -49 -60 -64 -57. -48 -27
14 -159 -33 -50
16 -104 -151 -36 -16 -4 -44 5
18 -143 2 -37
20 -103 -131 -27 17 12 -11 33
22 -100 18 27
24 -104 -74 -60 -40 -17 1 13 24 37 46 54 65 68
26 -104 18 35
L 28 -104 -138 -8 20 54 28.5 77
0 30: -139 7 30
N 32 -108 -122 -10 -5 50 32 91.5
G 34 -101 -4 44
I 36 -115 -113 -104 -85. -62 -36 -8 -7 -5 0 13 33 57 57.5 61.5 65 73 82 99T 38 -71. 8 70
U 40 -125 -73 -12 22 57 62 100
D 42 -91 36 58
E 44 -140 -107 -16 28 60 60.5 10046 -107 4 61
48 -15 -116 -99 -79 -36 -22 -8 5 49 69 76 83 110
50: -153 -2 59
152 -177 -193 -52 -3 42 41 90
54 -216 -15 18
56 -203 -235 -75 -25 44 2 83
58 -251 -41 -4
60 -230 -252 -265 -259 -227 -172 -101 -93 -80 -63 -43 -22 7 -11 -20 -15 4.5 34 70
62 -265 -78 -29
:64 -259 -277 -130 -81 -11 -33 53
66 -288 -88 -30
:68 -298 -287 -163 -102 -34 -31 34
70 -277 -116 -31
72: -335 -290 -264 -242 -199 -154 -138 -115 -71 -41 -24 -10 14
166
DISTORTION MEASUREMENTS OF 1/8" PLATE AFTER PANELS 5 AND 4 WERE LINE FLAME HEATED FOR THE FIRST TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -147 -136 -140 -135 -125 -128 -128 -125 -125 -115 -125 -127 -128 -140
2 -139 -152 -111 -103 -B5 -122 -1124 -135 -174 -99 -80 -70 -108 -90.6 -129 -191 -90 -70 -57 -85 -698 -125 -191 -76 -68 -41 -68. -48.
10 -123 -185 -65 -60 -28 -56 -3012 -121 -156 -182 -182 -155 -107 -57 -47 -44 -42 -37 -29 -18 -37 -46 -48 -40 -30 -1014 -123 -181 -52 -28 -34 816 -118 -171 -38 -12 4 -30 2418 -120 -156 -31 9 13 -23 3920 -122 -139 -33. 23.5 19 3 5422 -126 -111 -29 21 37 42 64
24 -126 -115 -92 -74 -51 -37 -26 -14 -2 11 26 44 55 59 69 82 9026 -127 -106 -21 17 50 49 96
L 28 -127 -128 -17. 18.5 61 44 990 30 -130 -132 -18 2 40 47 106.N 32 -131 -127 -17. -13 57 48.5 113C 34 -131 -114 -16 -10 62 61 116
I 36 -135 -128 -116 -95 -67 -40 -14 -9 -6 0 17 38 64 68 74 80 91 102 120T 38 -138 -73 -17 13 65 84 121U 40 -141 -66 -16 31 66 76 121D 42 -146 -78 -11 47 67 73 120E :44 -152 -94 -18. 37 69 75.5 121
46 -157 -101 -26 10 65 78 12548 -166 -122 -103 -82 -35 -27 -18 -3 13 60 83 92 101. 131
• .50 -171 -155 -34 6 67 76 11752 -179 -193 -45 7 55 38 11154 -189 -216 -56 -4 49 35 11056 -200 -233 -66 -13 58 20 103.58 -213 -248 -77 -28 14 9960 -224 -245 -259 -253 -219 -164 -91 -81 -68 -50 -29 -7 23 4 -3 2 24 54 9062 -236 -257 -101 -63 14 -12 8364 -251 -267 -117 -66 4 -16 7366 -264 -276 -134 -72 -8 -12 6568 -282 -273 -147 -85 -16 -13. 5370 -298 -261 -166 -98. -32 -14 4272 -305 -271 -245 -223 -201 -180 -135 -118 -96 -52 -23 -4 8 22 31
167
I.,
DISTORTION OF 1/8" PLATE AFTER PANELS 5. 4, AND 6 WERE LINE FLAME HEATED FOR THE FIRST TIME
TRANSVERSE...............................................................................................
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -145 -134 -138 -133 -128 -122 -126 -127 -122 -111 -122 -125 -126 -129 -1382 -136 -150 -109 -101 -84 -120 -1104 -132 -172 -97 -77 -68 -117 -896 -126 -187 -88 -67 -55 -88 -688 -123 -187 -74 -66 -39 -72 -49
10 -121 -182 -64 -58 -25 -64 -3112: -118 -153 -180 -181 -153 -105 -56 -46 -42. -41 -37 -28 -18 -39 -51 -54 -47 -34 -1114 -120 -178 -51 -26. -4 -40 6
:16 -115 -169 -37 -12 3 -31 21:18 -117 -153 -30 12 12 -20 35
20 -118 -137 -32 26 17 7 4922: -124 -109 -28 22 34 42.5 6024 -123-111 -90 -72 -50 -35 -25 -12 -3 10 25 38 41 50 55 66 77 86 8626 -125 -105 -20 16 48 60 92
L 28 -125 -125 -16 16 60 60.5 950 30 -127 -130 -17 -3 60 61 104N 32 -128 -124 -16 -18 58 57.5 111C 34 -129 -111 -15 -14 63 64 115I 36 -133-126-114 -93 -66 -38 -13 -8 -7 0 15 39 66 70 75 80 90 102 120T 38 -126 -71 -15 15 68 85 122U 40 -140 -64 -14 36 70 81 124D 42 -145 -77 -9 53 71 83 124E 44 -151 -93 -16 43 74 91 126
46 -156 -99 -22 15 71 91.5 13448 -165 -145 -121 -101 -80 -31. -22 -14 2.5 18 66 80 90 101 110 122 14050 -171 -153 -30 13 74 88 12752 -179 -192 -42 14 64 70.5 12454 -190 -215 -51 5 59 47 12456 -201 -231 -62 -4 69 33 12058 -214 -245 -72 -19 50 27 11660 -225 -245 -29 -251 -217 -158 -85 -74 -60 -40 -20 4 35 17 10 16 39 71 10962 -238 -255 -95 -53 30 4 10464 -251 -266 -111 -54 19 1 9666 -268 -275 -126 -60 8 7.5 8968 -284 -271 -140 -73 1 8 79.570 -300 -259 -158 -85 -14 10 7072: -318 -272 -244 -220 -170 -124 -104 -79 -58 -32 0.5 21 34 50 60
168
DISTORTION OF 1/8" PLATE AFTER PANELS 5,4,6,AND 2 WERE HEATED THE FIRST TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -138 -127 -132 -128 -122 -118 -122 -123 -119 -117 -107 -119 -121 -121 -125 -1332 -130 -145 -106 -91 -80 -117 -1064 -126 -168 -92. -65 -66 -105 -866 -121 -186 -85 -55 -53 -85 -658 -117 -186 -71 -54. -37. -71. -46
10 -115 -181 -61 -47 -24. -63 -28
12 -112 -149 -177 -179 -152 -103 -53 -39 -32 -29 -26 -22 -16 -39 -52 -56 -47 -33 -914 -115 -177 -13 -10 -43 916 -II0 -166 -36 7 4 -34 2318 -112 -152 -28 33 13 -22 3620 -114 -135 -31 49 18 5 5022 -120 -107 -26 39 34 42 6024 -120 -109 -87 -70 -48 -34. -23 -11. -3 11 25 38 42 51.5 56 65.5 78 88 8726 -120 -103 -19 21 50 60 92
L 28 -121 -124 -14. 21 60 60 950 30 -124 -130 -16 3.5 60 60 104N 32 -124 -124 -15 -8 59 56.5 111G 34 -126 -111 -12. -10 64 63.5 1151 36 -130 -123 -111 -90 -63 -35 -10 -7 -5 0 16 40.5 67.5 71 76 80 91 103 121T 38 -134 -68 -12. 15 70 86U 40 -136 -60. -11 37.5 71 83 124D 42 -141 -73 -5 54 74 85 125E 44 -148 -88. -13 45.5 76 92.5 127
46 1-152 -95 -19 18 73 95 13348 -161 -140 -117 -97 -76 -28. -20 -11 5 21 68.5 81 92.5 102 112 14150 -167 -149 -28 14 76 89 12952 -175 -187 -39 16 65 73 12554 -185 -210 -48 6 60 50 125
d 56 -196 -226 -58 -2.5 71 35 12158 -208 -240 -69 -16 51 30 11860: -220 -241 -253 -246 -212 -154 -81. -71. -55 -37. -15 7.5 38 21 14 19 42 74 110.62 -249 -91 -50 31 7 10664 -247 -259 -106 -52 22 4 9866 -262 -268 -121 -57 11 10 9268 -280 -264 -135 -70 4 11 82
:70 -295 -252 -154 -82 -11 13 7272 -312 -286 -265 -236 -213 -164 -118 -100 -76 -55 -28 4 23.5 39 54 64
a,1
.' .,,. ' £g.,I +2 e ". " € ".. e - ,-o' ""- " -;- --- --. " " -. ."169 , ,
DISTORTION OF 1/8" PLATE AFTER PANELS 5,4,6,2,AND 8 WERE HEATED THE FIRST TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36----------------------------------------------------------------------------------------------
0 -132 -124 -122 -126 -122 -117 -111 -116 -117 -113 -111 -101 -113 -116 -116 -120 -1282 -125 -140 -100 -85 -78 -112 -10241 -120 -163 -87 -60 -61 -101 -826 -115 -180 -79 -50 -50 -82 -638: -III -180 -66 -50 -33 -69 -44
10 -109 -176 -56 -43 -20 -62 -2812 -108 -143 -171 -174 -147 -98. -49 -35 -28 -25 -22 -18. -14 -37 -50 -54 -45. -32 -814 -109 -172 -44 -9 -7 -41 816 -103 -162 -30 10 6 -33 2218 -105 -147 -25 36 14.5 -21 3520 -108 -131 -27 51 19 5 4822: -113 -102 -23 41 36 41.5 5824 -112 -101 -80 -64. -44 -30 -20 -8 0 13.5 26 42 51 55.5 64.5 76 85 83
126 -113 -98 -15 22.5 49 59 88L 28 -113 -119 -11. 22.5 60 57 910 30 -116 -125 -13 4 60 57 99N 32: -116 -119 -12 -12 57 53 106G :34 -118 -105 -10 -10 62 60.5 109I:36:-121-116-15 -85 -59 -32 -8 -5 -4 0 15 39 65 68 72 76 85.5 98 114T 38 -125 -62 -10 14 67 81 116U 40 -127 -55 -9 35 69 78 113D 42 -132 -68 -4 50 70 78.5 116E 44 -138 -84 -11 40 72 85 118
146 -144 -91 -18 13.5 69 85 12548 -152 -132 -111 -93 -73 -28 -20 -12 3 18 63 75 85 94 102. 13050 -160 -144 -28 IB 69 80.5 11652 -168 -179 -39 29 58.5 65 Ill54 -179 -201 -49 26 54 42 Ill561 -189 -217 -58. 21 63.5 26 10658 -201 -230 -70 8.5 43 20 10260 -212 -233 -244 -236 -203 -149 -82 -57. -34 -14 1.5 12 30 11 3.5 8 29.5 59 9562 -225 -240 -92 -27 23 -5 8964 -239 -253 -107 -32 13 -7 8066 -253 -263 -122 -41. 3 -2 7368 -271 -261 -136 -60 -5 -2 6370 -285 -248 -154 -81 -20 -1 53
172: -302 -259 -233 -212 -189 -167 -123 -106 -83 -63 -38 -10 8 20 35 43
170
,>%%
DISTORTION OF 1/8" PLATE AFTER PANELS 5.,4,6,2,8, AND 3 WERE HEATED THE FIRST TIME
TRANSVERSE-----------------------------------------------------------------------------------------------
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36-----------------------------------------------------------------------------------------------
0 -124 -113 -118 -114 -109 -104 -110 -111 -107 -106 -96 -108 -110 -110 -113 -120
2 -114 -131 -91 -79 -71 -96 -98
4 -111 -155 -81 -51 -57 -75 -80
6 -105 -172 -72 -41 -46 -47 -62
8 -101 -172 -60 -42 -31 -28 -44
10 -100 -166 -50 -36 -19 -18 -28
12 -97 -133 -161 -164 -139 -91. -44 -29. -23 -19. -17. -15 -11 -6.5 -2 -5 -10. -18 -11
14 -99 -161 -38 -5 -6 10 516 -94 -152 -26 12 6 15 1818 -96. -137 37 15 18 32
20 -99 -121 -22 53 19.5 33 4622 -104 -94 -17 44 35 54 58
24 -103 -93 -73 -57 -37 -23 -15-3.5 5 17 29 41 43 51 65 64 75 84 84
26 -104 -91 -10 26 49 55 89
L 28 -105 -112 -6 24.5 60.5 54.5 92
0 30 -107 -117 -7 5 60 55 101N 32 -108 -112 -6 -13 58.5 54 108
G 34 -110 -98 -5 -10. 64 62.5 112
1 36 -114 -108 -97 -78 -51 -25 -2.5 -1.5 -4 0 15 40 67 73 78 81.5 92 103 118
T 38 -118 -55 -5 16 69.5 88 120U 40 -121 -48 -4 38 71 84 121
D 42 -127 -61. 1 55 73 85 121
E 44 -133 -79 -6 46 76 91 12346 -138 -86 -13 18.5 73 91 130
48 -147 -126 -105 -87 -67 -22. -14 -7 8 23 68 81 90 100. 109 137
50 -152 -131 -21 25 76 88.3 12552~ -161 -174 -32 36.5 66 73.5 12
54 -172 -195 -42 34 61.5 51 121
56 -183 -209 -52 29 72 35 116.
58: -195 -224 -62. 15.5 52.5 29 113
60 -207 -227 -238 -229 -197 -143 -75 -50 -26. -6 10 21.5 39 21 13 18 39 69 105
62 -220 -232 -85 -19 33 7 10064 -233 -247 -100 -23. 24 3 92
66 -249 -257 -115 -33 12 9 85
68 -267 -255 -130 -52 5 10 75
70 -282 -243 -147 -71 -10 11 65
72 -301 -254 -227 -204 -182 -159 -114 -96 -73 -28 2 21 33.5 48 57
171
DISTORTION OF 1/8" PLATE AFTER PANELS 5,4,6,2,8,3,AND I WERE HEATED THE FIRST TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -76 -78 -89 -90 -90 -88 -96 -98 -95 -94 -85 -98 -100 -101 -104 -111
2 -76 -100 -78 -66 -60 -86 -894 -81 -130 -68. -38 -47. -64 -696 -8'. -160 -63 -28 -33 -36. -508 -86 -176 -53 -30. -22 -17 -3310 -90 -185 -45 -24 -10 -7 -1712 -92 -141 -184 -192 -157 -92 -40 -17 -6 -4 -6 -6 -3 1.5 8 6.5 3 -4 314 -98 -188 -37 13 2 19 18
:16 -97 -165 -24 33.5 14 23 3318 -100 -134 -19 60 23 26.5 4620 -104 -110 -23 73 28 42 6022 -108 -84 -18 55 44 64 71
24 -105 -94 -74 -59 -35. -24 -16 -3 7 19 34 47 50 60 66 75 89 99 9826 -103 -89 -10 25 58 68.5 104
L 28 -I01 -108 -4.5 22.5 68.5 68 1070 30 -I01 -109 -4 -1 68.5 70 116
N 32 -I00 -99 -2 -20 67.5 69 123G 34 -99 -83 2 -16. 73 78 126I 36 -101 -93 -81 -63 -37. -15 4.5 4 -1.5 0 18 47 77 84 91 96.5 104. 116 131T 38 -103 -41 3.5 21 80 101 133U 40 -104 -34 6 49 82 96 133D 42 -108 -47. 13 68.5 84 96.5 133E 44 -113 -64 7.5 60 88 102. 134.:46 -117 -68 2 33.5 86 102. 1411 48 -125 -104 -84 -67 -48 -6 2 8 23 37.5 81 93 102. 112 119. 130 147
50 -128 -116 -3.5 40 89 99 13352 -135 -151 -14 53 80 85 12954 -144 -170 -21 51 75 63 12956 -152 -184 -30 47 88 48 12458 -163 -196 -39 35.5 68 42.5 119.60 -173 -194 -207 -201 -169 -113 -50 -26 -3 15 29 39 54 36 27.5 31.5 52 80 11262 -183 -203 -59 2 48 19 10664 -196 -214 -73 -2 40 16 9866 -207 -223 -86. -10 30 21.5 9168 -225 -218 -99 -28 23 21.5 80
1 70 -238 -204 -115 -46. 9 22.5 70
:72 -252 -212 -187 -166 -147 -125 -86 -70 -50 -32 -8.5 16 32.5 42 55 61
172
P
DISTORTION OF 1/8" PLATE AFTER PANELS 5.4,6,2,8,3.1oAND 7 WERE HEATED THE FIRST TIME
TRANSVERSE...............................................................................................
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36...............................................................................................
0 -56 -58 -67 -67 -66 -64 -71 -73 -70 -68. -59 -71. -74 -74 -77 -85
2 -56. -78 -56 -41 -35 -61 -624 -61 -108 -46. -15 -23. -40 -466 -63 -139 -42 -7 -14 -14 -28.8 -66 -155 -32 -10 0 5 -12.10 -69 -164 -25 -5 10.5 14 2.5
12 -72 -122 -166 -174 -139 -74 -21 3 13 15 13.5 13 15 20 25 24 19 13 1914 -78. -171 -17 32 19.5 36 33.516 -76 -148 -6 52 30 38.5 4718 -80 -118 -2 77.5 37 39 59
20 -83 -93 -6 90 40 53 7122 -87 -67 -3 69 56 74 8024 -83 -75 -57 -42 -20 -8.5 -1 10 19 31.5 45 58 61 70 74 84 96.5 106 10626 -81 -71 3.5 36 67 75.5 Ill
L 28 -79 -89 9 31 77 76.5 1120 30 -78 -90 8 2 76 77.5 119N 32 -76. -80 9 -21 73 75 124G 34 -75 -65 12 -18 78 82.5 126.
I 36 -76. -72 -64 -47. -25 -3.5 14.5 9 0 0 18 48 81 87 93 96 105 114 130T 38 -78 -30 13 28.5 82.5 98.5 129.U 40 -79. -27. 14.5 62 84 91 129D 42 -83 -42 21 85 85 92 126.
E 44 -88 -55 15 72). 5 88 96 12646 -91. -56 9.5 39 85 96 131
48 -99 -65 -52. -37 2 8 12 26 39 79 97 IA 110 118 133.50 -103 -97. 6 45 83 90 11852: -107 -133 -3.5 63 76 73 11054 -112 -156 -9 65 71 49 10756 -119 -189 -16 64 81 32 10058 -124 -198 -23 55.5 62 24 9360 -'.28 -164 -197 -203 -168 -102 -32 -3 20 35 41 41 49 23 10.5 11 28 52.5 8362 -133 -199 -37. 22 43 -2.5 7464 -138 -197 -48. 20 35 -7 6266 -143 -186 -59. 11 24 -2 52
68 -152 -164 -69 -9 17 -3 3970 -156 -141 -81 -31 2 -3.5 25
72 -163 -141 -126 -114 -102 -90 -64 -55 -41. -31 -15 -4 5 8 13 13.5
173
• ".' .' " ," .'. -. ' ''.' ' . " ". '.. .. " .. .'..".. .- . % . " . .' " 5- -,• •• - .. • .J .. ., . ... ~ ~' ~'S .5 . . ...
DISTORTION OF 1/8" PLATE AFTER PANELS 5,4,6,2,8,3,1,7,AND 9 WERE HEATED THE FIRST TIME
TRANSVERSE-----------------------------------------------------------------------------------------------
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36-----------------------------------------------------------------------------------------------
0 -44 -45. -54. -55 -53. -51 -58 -59. -56 -55 -46 -57 -60 -60 -63 -70
2 -45 -66. -43 -29 -22 -47 -49
4 -50. -96. -34. -2 -10 -27 -32
6 -53 -127 -30 5.5 0 -1.5
8 -57 -144 -21. 1.5 12.5 17.5 1.5
10 -61 -154 -14 7 23 26 16
12 -64 -113 -158 -165 -130 -65 -11 13 23 26 24 24 27 31 36.5 35.5 32 25 33
14 -70. -164 -9 44 31 47 47
16 -69 -142 2.5 63.5 41 50 60
18 -73 -111 7 89 46 51 72
20 -76 -87 1.5 100 50 64 84
:22: -82 -61 5 78.5 65 85 94
24 -78 -70 -51 -35. -14 -3 6 17 26.5 41 52.5 65 70 84 95 108 118 119
26 -76 -66 11 43 75 86 123
L 28 -74. -84 14.5 36 85 87 124
0 30 -74. -85 13.5 5 83 89 132
N 32 -73 -75 14.4 -20 79 88 136
G 34: -73 -60. 16.5 -18 84 95 138
I 36 -74. -70 -61 -44 -22 -1 19 11.5 1 0 19 51 86 94 102 108. 115. 124. 140
T 38 -76 -27 16 30 87 108 140
U 40 -79 -25 17 65 88 97 139
D 42 -82 -40 23 88 88 93 136
E 44 -88 -55 17 75 91 96 135
46: -92 -56 11 41 88 96.7 140
"48: -101 -85 -66 -53 -37 2 9 14 27 40 81 93 100 107 115 141
50 -105 -98 6 47 87 106 122
52 -110 -134 -4 65 77 103 116.
54 : -117 -157 -10 68 72 83 112
56: -123 -180 -17 68 82 63.5 106
58: -129 -201 -25 58 62 50 99
60 -134 -169 -202 -206 -171 -106 -35 -4 22.5 40 47 45.5 50 38 28.5 29.5 44.5 65 89
62 -139 -205 -41 29 43 12.5 82
64 -146 -202 -51 29 36 11 72
66 -152 -194 -62 20 25 23.5 65
68: -161 -171 -72 -4 20 24 54
70 -166 -148 -85 -28 5 17 43
72: -172 -149 -132 -120 -106 -93. -65 -55 -40 -28 -10 4 16.5 22 31 34
t174
APPENDIX G
1/8" STIFFENED PLATE OUT-OF-PLANE DEFLECTION READINGS
RECORDED AFTER LINE HEATING THE 2ND. 3RD. AND 4TH PASS
Appendix G contains 8 sets of out-of-plane deflectionmeasurements. The first 4 are for the 2nd heating pass, thenext 2 are for the 3rd pass. and the last 2 are for the 4thpass. See Table 2-2 for the line heating sequence of eachpass.
NOTE: In appendixes D, E, F, and G the TRANSVERSE andLONGITUDE spacing is 2 inches. All deflection readings in thematrixes are in .001 inches. For example, the out-of-planedistortion at 10 inches TRANSVERSE and 2 inches LONGITUDE, inthe matrix labeled "DISTORTION MEASUREMENTS OF 3/16" PLATEAFTER WELDING" is -0.075 inches (i.e. 0.075 below thereference point). This point is designated D(6,2) as it ison the 6th line in the TRANSVERSE direction and the 2nd linein the LONGITUDE direction.
1 75
w ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 2 AZ: %2"--~ ~5- ...5. . ** .- -**.*.
wf p- r sm X" KRI - flhn VWrW WL rr, M Lrw Vun v-VI uwv r irJYvlnn
DISTORTION OF 118" PLATE AFTER PANEL 5 WAS HEATED THE SECOND TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -141 -153 -149 -159 -146 -161 -172
2 -164 -128 -1484 -196 -102 -126
6 -227 -96 -98
8 -245 -100 -7910 -257 -94 -70.
:12 -162 -213 -259 -268 -233 -165 -112 -87 -76 -75 -77 -78. -76 -70 -63 -62 -65 -73. -69
14 -266 -57 -5316 -245 -38 -5318 -215 -15 -54
20 -190 -7 -42:22 -164 -31 -2124 -179 -138 -98 -65 -35 -8.5 16.5
:26 -167 -46 -10
L 28 -184 -26 -4.5
0 30 -185 -27 2.5
N 32 -176 -31 1G 34 -163 -18 31 36 -176 -172 -164 -148 -127 -106 -85 -44 -11 0 -5 -16 -19 -6.5 6 12.5 18 24 38
T 38 -132 14 10U 40 -127 26 -1D 42: -140 24 -6
E 44 -154 -10 -546 -156 -58 -8
48 -201 -154 -101 -77 4 3950 -201 -59. -24 11.5
52 -239 -43 33
:54 -264 -43 4756 -285 -46 5758 -304 -59 5960 -232 -269 -303 -309 -274 -207 -137 -112 -91 -80 -75 -72 -56 -35. 3 37 51 31 -17
:62 -305 -89 164 -303 -86 -27
66 : -293 -91 -45
:68: -271 -111 -67: 70 -248 -134 -8772 -269 -233 -196 -160 -117 -94 -77
176
i-l KS
-. :
DISTORTION OF 1/8" PLATE AFTER PANELS 5 AND 4 WERE HEATED THE SECOND TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -127 -139 -136 -146 -133 -148 -1582 -151 -116 -1354 -182 -91 -1156 -213 -84 -87a -231 -89 -6910 -243 -83 -60.12 -148 -199 -246 -254 -221 -155 -101 -76 -65 -63 -65 -68 -66 -61 -54 -54 -57 -65 -6014 -255 -45 -4516 -236 -26 -46
i 18 -206 -4 -4820 -182 3 -35
:22 -155 -21 -15:24 -164 -127 -88 -57 -28 -3 2126 -153 -40 -6
L 28 -164 -23 00 30 -156 -28 7N 32 -141 -34 5G 34 -124 -20 8I 36 -162 -150 -131 -110 -92 -83 -78 -39 -10 0 -4 -14 -15 -3 9 5.5 19 23.5 37.5T 38 -96 18 11u 40: -97. 32 -2D 42 -116 31 -8E 44 -136 -4 -7.5
46 -143 -54 -1148 -183 -143 -93 -74 -24 0 3250 -191 -55 7
:52 -228 -37 2854 -251 -36 41
56 -271 -40 5058 -288 -54 5160 -209 -247 -283 -291 -258 -194 -127 -103 -86 -77 -73 -72 -57. -39 -2 30 41 19 -3062 -285 -88 -664 -282 -84 -3566 -272 -88 -54:68: -250 -108 -7770 -227 -130 -9972 -240 -211 -182 -155 -122 -107 -100
177
"-''-
-IKk t I SM LFWL" L w lS Wn-w IT SWW
DISTORTION OF 1/8" PLATE AFTER PANELS 5,4, AND 1 WERE HEATED THE SECOND TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -128 -141 -139 -148 -135 -151 -1612 -144 -117 -1384 -167 -92 -1176 -199 -86 -908 -218 -92 -71I10 -231 -87 -63
1 12 -154 -195 -233 -238 -206 -148 -106 -81 -69 -67 -69 -71 -69 -64 -57 -56. -59 -62. -62
14 -228 -49 -4816 -198 -29 -4918 -166 -6.5 -5120 -150 0 -3922 -138 -25 -1824 -170 -132 -93 -61 -31 -6.5 17.526 -156 -44 -10
L 28 -166 -28 -20 30 -159 -32 5N 32 -145 -35 2.5C 34 -130 -21 4I 36 -167 -154 -136 -115 -97 -87. -82 -41 -11 0 -4.5 -16. -18 -6 6 11 16 21 35T 38 -101 16.5 7U 40 -101 30 -5D 42 -120 28 -10
E 44 -140 -6 -1046 -146 -56 -13
.48: -184 -146 -96 -76. -26 -2 30o50 -194 -58 6
.52 -230 -40 27,54 -254 -38. 40
56: -273 -42 4958 -291 -56. 5060: -211 -248 -285 -294 -260 -196 -129 -105 -88 -79 -76 -75 -61 -41 -4 28 39 17.5 -3262: -288 -89 -864: -284 -86 -3866 -275 -91 -5668 -251 -109 -7970 -228 -131 -10172 -243 -213 -184 -158 -125 -109 -101
do 178
DISTORTION OF 1/8" PLATE AFTER PANELS 5.4,1, AND 7 WERE HEATED THE SECOND TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -131 -145 -141 -151 -138 -153 -162
2 -147 -121 -1404 -170 -94 -1196 -202 -88 -92
8 -221 -94 -7410 -234 -89 -612 -156 -198 -236 -240 -209 -150 -108 -83 -71. -70 -72 -73. -71 -66 -59 -59 -62 -70 -65.14 -230 -51 -5016 -201 -31 -5218 -169 -9 -5420 -152 -2 -4222 -140 -26. -21
24 -172 -134 -95 -63 -34 -9 1526 -158 -46 -11
L 28 -169 -29 -50 30 -162 -31 2N 32 -148 -34 -1G 34 -132 -20 1I 36 -169 -156 -138 -117 -100 -90 -84 -43 -11 0 -4 -18 -21 -9.5 2 8 13 18 31T 38 -103 16 4
U 40 -102 28 -8D 42 -119 25 -14E 44: -138 -10 -13
46: -145 -59. -16.48 -188 -148 -99 -79 -29 -5 25.550 -178 -59 252 -203 -40 2354 -222 -39 3756 -248 -44 4658 -274 -59 4760 -212 -247 -279 -286 -255 -194 -132 -108 -91 -82 -78 -77 -63 -44 -7 25 37 14 -3662 -284 -91 -1264 -278 -87 -4166 -264 -90 -59
68 -240 -110 -8270 1 -221 -133 -104
72 -241 -214 -186 -159 -126 -111 -105
179
DISTORTION OF 1/8" PLATE AFTER PANEL I WAS HEATED THE THIRD TIME
TRANSVERSE----------------------------------------------------------------------------------------------
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -131 -145 -143 -154 -141 -156 -1662 -143 -122 -1434 -161 -95 -1236 -185 -88 -958 -198 -94 -7710 -204 -89 -7012 -158 -185 -206 -202 -174 -132 -111 -85 -72 -70 -72 -75 -74. -69. -63 -63 -66 -72 -68.14 -186 -52 -5516 -156 -33 -5618 -134 -12 -57
2'. 20 -129 -6 -44.:22 -130 -30 -23.
24 -174 -137 -98. -66 -36 -12 1226 :-162 -49. -14
L 28 -174 -32 -80 30 -167 -33 -2N 32 -153 -34 -5G 34 -136 -19 -3I 36 -171 -159 -140 -120 -103 -93 -88 -45 -11 0 -5 -19. -23 -12. -1 4 9.5 15 28.5T 38 -105 15 0U 40 -104 26 -12D 42 -121 22.5 -17E 44 -141 -13. -16
46 -148 -63 -2048 -191 -151 -102 -82. -32 -8 23.550 -183 -63 -152 -207 -43 2154 -226 -42. 3456 -252 -47 4358 -279 -62 4460 -216 -251 -283 -289 -260 -199 -135 -112 -94. -85 -82 -80 -66 -47 -10 22 34 11 -3862 -287 -94 -1564 -282 -90 -4466 -268 -93 -6268 -244 -112 -8570 -225 -136 -10772 -246 -218 -189 -162 -130 -114 -106
S18
1%%%
DISTORTION OF 1/8" PLATE AFTER PANELS I AND 7 WERE HEATED THE THIRD TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -132 -148 -145 -155 -142 -158 -1682 -144 -123 -145
-162 -96 -1246 -186 -90 -97
8 -200 -96 -78.1 I0 -205 -91 -71
: 12 -158 -186 -207 -203 -176 -133 -113 -87 -74 -71 -74 -77 -75 -71 -65 -65 -68 -76 -71:14 -187 -53 -56.
16 -158 -35 -5818 -135 -13. -5920 -130 -7.5 -4722 -131 -32 -2624 -175 -138 -IOC -68 -38 -14 1026 -163 -51 -17
L 28 -175 -34 -100 30 -169 -35 -4N 32 -155 -36 -7G 34 -139 -20 -6I 36 -172 -160 -143 -123 -106 -96 -90 -46 -12 0 -6 -21 -26 -15. -4 1.5 6 12 25.5T 38 -107 15 -2.5u 40 -105 25 -14D 42 -121 21 -19E 44 -139 -16 -19
:46 -146 -65 -22:48 -191 -152 -104 -84 -33 -10. 20.5:50 -166 -62. -3.552 -176 -42 1754 -187 -41 3156 -213 -48. 4058 -247 -66 4160 -212 -238 -264 -267 -239 -187 -136 -115 -99 -89 -85 -82 -68 -49 -12 19 31 7.5 -4362 -273 -98 -1764 -271 -91 -4666 -257 -92 -6568 -232 -111 -87.70 -214 -135 -1I0
72 -236 -212 -186 -161 -129 -117 -113
1 81
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DISTORTION OF 1/8" PLATE AFTER PANEL 7 WAS HEATED THE FOURTH TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
%'I
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A 24 -175 -139 -101 -69 -39.26 -164 -52.
L :28: -176 -340 30 -170 -35N 32 -156 -35" 34 -139 -191 36 -172 -160 -142 -123 -105 -96 -91 -48 -12 0 -5.5 -21 -27T 38 -106 14U 40 -104 24- 42 -120 19E 44 -138 -17
46 -146 -6848: -191 -154 -105 -85. -3550 -155 -62.52 -159 -4254 -165 -4156 -186 -4958 -219 -6660 -211 -227 -242 -241 -216 -175 -135 -116 -100 -90 -86 -84 -6862 -250 -9B64 -250 -9066 -239 -9168 -217 -10970: -204 -13472 -232 -209 -185 -161 -131
182
I.
DISTORTION OF 1/8" PLATE AFTER PANELS 7 AND I WERE HEATED THE FOURTH TIME
TRANSVERSE
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36
0 -134 -150 -147 -157 -145
2 -143 -1264 -155 -996: -172 -93
8 -177 -10010 -173 -9612 -163 -172 -174 -164 -144 -118 -116 -90. -77 -74 -75 -78 -7814: -148 -5516: -125 -34
. 18. -113 -12:' 20 -117 -71 22 -125 -33.24 -180 -142 -103 -69 -40..26 -166 -54
L 28: -177 -370 30: -171 -37N 32 -156 -36G 34 -140 -19I :36 -176 -164 -146 -125 -107 -97 -91. -47 -12 0 -6 -21 -27.T 38 -109 15U 40 -107 24D 42 -123 19E 44 -140 -17
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APPENDIX H
GRAPHS OF THE 3/16" STIFFENED PLATE MID-PANEL DEFLECTIONSAFTER THE FIRST LINE HEATING PASS
The horizontal coordinate is transverse or longitudinaldisplacement. measured in inches. and the vertical coordinateis out-of-plane deflection. measured in thousandths of aninch.
418
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APPENDIX I
GRAPHS OF THE 3.,16" STIFFENED PLATE MID-PANEL DEFLECTIONSAFTER THE SECOND LINE HEATING PASS
The horizontal coordinate is transverse or longitudinaldisplacement. measured in inches. and the vertical coordinateis out-of-plane deflection. measured in thousandths of an Q
inch.
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APPENDIX J
GRAPHS OF THE 1/81 STIFFENED PLATE MID-PANEL DEFLECTIONSAFTER THE FIRST LINE HEATING PASS
The horizontal coordinate is transverse or longitudinaldisplacement. measured in inches. and the vertical coordinateis out-of-plane deflection. measured in thousandths of aninch.
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GRAPHS OF THE 1.,,8" STIFFENED PLATE MID-PANEL DEFLECTION'AFTER THE SECOND LINE HEATING PASS
The horizontal coordinate is transverse or longitudinaldisplacement. measured in inches, and the vertical coordinateis out-of-plane deflection. measured in thousandths of aninch.
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GRAPHS OF THE 1/8" STIFFENED PLATE MID-PANEL DEFLECTIONSAFTER THE THIRD AND FOURTH LINE HEATING PASS
The horizontal coordinate is transverse or longitudinaldisplacement. measured in inches, and the vertical coordinateis out-of-plane deflection, measured in thousandths of anin ch.
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APPENDIX M
GRAPHS OF THE 3./16" STIFFENED PLATE TRANSVERSEOUT-OF-PLANE DEFLECTION READINGS FOR LINES
AD2 THROUGH AD7
The horizontal coordinate is the transverse displacement.measured in inches. and the vertical coordinate is out-of-plane deflection. measured in thousandths of an inch.
237
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APPENDIX N
GRAPHS OF THE 7.!16" STIFFENED PLATE TRANSVERSEOUT-OF-PLANE DEFLECTION READINGS FOR LINES
AD7 THROUGH ADi2
The horizontal coordinate is the transverse displacement.measured in inches, and the vertical coordinate is out-of-plane deflection. measured in thousandths of an inch.
m.
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Sm..0
.4 4
'I IIf-
3-l
2484
Q
*r LO
I w4- I-
LO
<0 0
UZIP
LILI
N 0 00 I'0I N N00 00 C,
IV
'24
Te
4.
'-'-.-I T
__T1)1 3I ' 0 I
IN' _o 1 N - -0 0 , I + <
250q
Lii,,..,
. -- I - - -
-. '-
.D. Li _
-- L --
.- - - '-A ', ¢l " '
-- --.-. ItO - L4---4- -
S aj
- 5
"w, ,l ." "+ "" "" % ''''' " °' . . . " '" ""'- " " *'-. . . . . . ,'"" • .- '''. " ' .+ "" " "+ . - ."'" "" ''. ","".' . ,'-'4", " ' ," J, " . P +' " '" *
'" " " * -. a % ." ' . " . " e . + . " .. " ., e . - . . ,..,.o++. " . . - . " .'
A F'FEND I 0
GRAPHS OF THE 71" STIFFENED PLATE TRANSVERSE
OUT-OF-PLANE DEFLECTION READINGS FOR LINESEH: THROUGH EH7
The hcrizzrtal zoordirnate is the transverse displacemerit.nmeasured in inches. an-d the vertical coordinate is out-of-
±a-Lne deflection. measureJ in thousandths of an inch.
I25
CC
Liij
LL- M
LL1
mj 04
CLC
-- 4-
(S H) I w NU-
I 252
I-Ltw
L (I
0
LLu
<'
LJ
- -f
it
~~~F 4 0'~ i
0 0 0 0 CI 0 i 0 )0 00k
p(S]H:DNI M'o) NI1 O D A
253
Li
X
*Z LJ-* . L L' L)
'LfJ
z 't
d70
4 4
a0
zw
(q-Hp-.N L- --
.254
'4~ 1-
iL
-' - 7
* NJ
LAY1 1 1 /
'I L -,-
LUj
25
~v uu ~~r T ~. ~'~~u~ ~ ~ ~ - jV ~ ~ v~ . ~ ~ xw.~ . : ~w'wLJ gw q
111 1ffEf L
- L
L__ _
cZ 0 C). I 0 I0ii 03 I4 C 3-
(S3H..)N 04 O :-TA3
JLL..........................
Lp -e
4- - W. -W.4-*- wv I- - 4-
LI
kL
L;~ 7
~'U W VU ~w U W WV w""V WWUUWVUUW Vw 33 PwWIA 117,01 MR7 Kn IM U*Y ir W W r~ %i 7~ 11W~ WKA .'v WW 'e i V - W ' R5Ms
APPENDIX P
GRAPHS OF THE 3/16" STIFFENED PLATE TRANSVERSEOUT-OF-PLANE DEFLECTION READINGS FOR LINES
EH7 THROUGH EH12
The horizontal coordinate is the transverse displacement.measured in inches. and the vertical coordinate is out-of-plane deflection, measured in thousandths of an inch.
258
- * $ X -' 'i '"U P, :'. '... .a 4h .'... . ..- ' C, k..x,
-_, LC ,eVVvW%*
C.-.
C) w
LL -L
z
LLL
0 a 0a 00m 0 N Q
(S3HDNI 00' N~l,-)3(A3I
259
C I
0 < zI
Li
Laiw
AI-
<Q)ON WO)NOI):n:(
26
I-l I
K i LU
0 QU
Al z
0 tOLLL
LLU
z it
(00
-9 w- ------ 0 +
(S3 HO NI L 00Y) N011O331J30l L
261
o M
wwFi XI
w
4M
0 u
Z1Lj
L--------L 0 23
LJ ii
ZZ
CL LLi
N. 0 m0 0m 0N
/ LiiI
w -
< VI
Lii~
LL __Ol
r1)
n 4
4 /D4N N4(Dw0N <
(SHN LO )
263
rvwlwrwvrlwlrFWWVPWTVVV MV WWM~v Lrwlmw wv~lm wtv- ITUVvwv v V v'Nx
o CA
Lii
ILL I
LL W
z 4
% 4 / ,F-IT
\II
0 W+N0mQ0
V- - #* -e-- --
(sJ3HONI LOU) NOIDJ3-1-JG wi
264&
APPENDIX 0
GRAPHS OF THE 3/16" STIFFENED PLATE TRANSVERSEOUT-OF-PLANE DEFLECTION READINGS FOR LINES
IL2 THROUGH !L7
The horizontal coordinate is the transverse displacement.measured in inches. and the vertical coordinate is out-of-plane deflection, measured in thousandths of an inch.
265
-.
-- J
U LLJ'I
z wQ).
fL 4.!
L.\'.
z )1Ld QI
< t'i
I~~~~~T N -'' -- ~~(J'
(S&3HCJNI L~OU) NOliOC31lAAL
266
Li
'9 < -
P9.d
zI
L I w
W /Jz I
((' 0.. 0 00 0
<0 -N N, <0 -n N Q-00N
(SHD ILU)Nr -) -
.267
LI~
W0<Q
/x
"4 -
IL
Liliz 0 -
K)1
TT--Tr0 00a 000 0a0
(q-]H:DNI 100o) NCli,-ICTJ]3J
268
NI - -A
MM t2i z Qr)
LLI ih
C<
(S~gHZ) I (SJ
'.A
LiJ
LL ZI
]I3 Ld
ILI
'LU
L
z .. , I
4 0 00Iq0a
.5.H)N \ * \ \ -. 3--J (
.- *.270
LL-J
wwNcrj
o4f
(S3 HO NI~ L 0' lO-I3
271d
M.~ w Fi w~rw -min ROOM IM Mr U.J WTkW~r- WW.'1rj --7 J VV VU .. w-~ ~-.~.p~~ ~ . ~ W1 y ~
APPENDIX R
GRAPHS OF THE 3/16" STIFFENED PLATE TRANSVERSEOUT-OF-PLANE DEFLECTION READINGS FOR LINES
IL7 THROUGH ILIL
The horizontal coordinate is the transverse displacement.measured in inches. and the vertical coordinate is out-of-plane deflection, measured in thousandths of an inch.
272
LJI
LL z Lii
LLii
zz
4 /Q)
j I I i(S3H NI IOO) QLL2J-U2I I I I I>
273
A(
ww
F -
0 w
C__ z /
wwCL,
27
T T1~1 I M J W PT mp rqp unW~ UWW L PW U I W ~nW IYW V W q V" UT LIV U W W TNWV- WMw
H--j
LLU
. -1
I-I
0 0 "D 00 004
275-'1,L
Wlwvq VwL ,L W11 VIIR 'n . -% .
K IC
F-:N
m S 0
_J £Ii -o
- Zi>
zz
0 m)
(SJHCJNI LOO) NOiDTU3JG(
276
LL-J
WQI- ~~0 -
1, (
zzCL4
40
N 8 3<(Srz)N M dr)l,3-Jr
----- 7-
tVT77
Li
00
D N 0 w'C
(SH* N LO )NkA09A3
W278
APPENDIX S
GRAPHS OF THE 3'i1" STIFFENED PLATE LONGITUDINALOUT-OF-PLANE DEFLECTION READINGS FOR LINES
AM- THROUGH AM6
The horizontal coordinate is the lonaitudinaldisplacement. measured in inches. and the vertical coordinateis out-of-plane deflection, measured in thousandths of aninch.
2
279
U- 4
LIJ LL1
LLI~X
zc 4Ld
D
~~-F 0-~
280
-AllI
<17LLJ ,
- 7.-
..... "
W1
ILL
L J", " - . - .... -
4-H
0L ' I '0L
f ^- I <0"3 l- N ." <A "f'-
81. .
I..-, ii..---- -l+
,
_. "N'>J .4 i ii - ' Ac i _ _c -
I I I I, I II : . .....
j,/ .., .....-.- ..-- .281_
zwnI
04
0 0 0 00 0 CD 0 a0 0 a I
(S H'-- -- - - )- -N- -L- -'- -li)3lA
2821
4-J
ILLJ
1' -'
1-7
<Ici
liJz
-ci
(0) -,' +^j0 Ia ) -f iN 0 " D NN
-" -l -N 'N
I.C-, a1 7 14L
283
Li)
-
z
LIMI
z LLI
z 0
IL
-2 'N <
K) -2
Er*
(S3 H3DNI L00') NC)Ji--ITJ30
284~
S'
LLf
LLii
zzn4z
285
APPENDIX T
GRAPHS OF THE 3/16" STIFFENED PLATE LONGITUDINALOUT-OF-PLANE DEFLECTION READINGS FOR LINES
BN2 THROUGH BN6
The horizontal coordinate is the loncitudinaldisplacement. measured in inches, and the vertical coordinateis out-of-plane deflection, measured in thousandths of aninch.
286
J-
1%,
0IL O%
*1-k x , *
2Mu LF
T111 1r:E
LLi
LLI
zz
-0
6J m
0 G ) 0 a 00 a a a0 a a+
(SHNsM )NOC)g-A(
287
sWvrp w v- Ulf nJ R M WV 7w' W VW r UrS-.w ww - w
cIIA
Li -
o z
-,Z z
__J z
zz
m
+
(S3H3NI LOU0) NOUII)ThJ
288
(33
* z
wN
-
ni
4
'
zici
*-N - -w- - -
4SK)N M ') -wi,)-I
z289
44'
(3:i
IJ
L9
290
I V.
Lii.
Til11rr
LLL
-7,
IdO
PIC
-70 0-Z C D a0a00
cL3HO-- LOU -Cl-D-J
~ cvi
Ll+
WSW W M Wf LFrWflVs SUl WVsf l lnl UWVrVV I FSf r rnf W-
4,'A4%
e ®r.'
'a-
*55
'as I
LLaJz~ [a
L)
C-
(S3H Nl M' NOU 3ItA3
292
v.-W WKU ViW iWVWV q! ~' % U- &r Mw j1 ~ VJ ~4 I-, VTR I~ q MT
%J. %41
APPENDIX U
GRAPHS OF THE 3/16" STIFFENED PLATE LONGITUDINAL
OUT-OF-PLANE DEFLECTION READINGS FOR LINES
CO2 THROUGH C06
The horizontal coordinate is the ,onaitudinal *- .-
displacement. measured in inches. and the vertical coordinateis out-of-plane deflection, measured in thousandths of aninc h.
N
2.9 .3'
.*% .1%
SF'
- J.-.
* , *.*.,*,~**~* *.'*,"* -* Np. ~ *,*** *.* .,,_
ji
00
LLIL
LJ L~Z
0
~zzo
SF- C0
LIwo
Q 0
(S3 :) I L CO N 0 i- TIA3 I
... 294
TTa
Lijw.L Lfl
LI
00
LLJ
z0CL
0
a a 0o00oao 0 0 a0 0o 0 0
(S3HZDNI iWOc) N(.)iC-jJ3.
295
.. 6
_j ~p~W-J
LJO
wi
CL~i
ISH-N M5)N~i,)lA(<H Xd
29
1X-
Ww
--
I% %
I( 1 0
I- _
z _4
Lii O
z Cz
z IAl
(L4
(S3 Hz-jNI iOO*) NOLLDc791i3
298I
x NA
Ld
w -as,
ZWN7F-~C __D 0a C__ __ _ _ _-
KSH.N ".4.NU0 J3
x299
APPENDIX V . .'-
3/16" STIFFENED PLATE MID-PANEL DEFLECTION DATAD(MAX)iT AND D(MAX)iL
,
This appendix contains the mid-panel deflection data,D(MAX)iT and D(MAX)iL. for the 3/16" stiffened plate. Thedata is in tabular form. All deflection readings are inthousandths of an inch. See Figure 3-2 for the definition ofD(MAX)iT and D(MAX)iL.
• . '4
%4 % * m3.0
:,
.+ -f
-. Cj
.p •° - . .
300€%'4
II -" .
.Jk
3/16" PLATEOut of plane deflection at the center of panel i. referenced to thetransverse straiQht line connecting the mid points of that panel',-;lonoitudinal stiffeners. See Figure 3-2 for the Definition, of D( MAX )iT. .
PANEL ,:HEATED$ !D( MAX )IT'D(MAX )2T:D( MAX )3T:D(MAX )4T:D'MAX )ST:D(MAX )6T:D(MAX)7T:D(MAX )8T;D(MAX)?T:
F WELD 63.5 63.5 55 58.5 63 53.5 60.5 51.5 70.5-I #5 71.75 96.75 52 46. 25 33.25 42 64 74.5 74R #4 68 88.5 51.5 -56 36.5 43.75 63 69 68S #2 55 62.5 42.5 -55.25 47 46.5 62.5: 65 66:T #8 55 60.5 43.75 -56 58.5 40 49.5 23.5 67:
#6 54 63 47 -51 46.5 38.5 49 25.5 61.5:P #1 39.5 55 47.5 -54 49.5 38.5 48 23.75 60.75A #7 40.5 55 47 -55.75: 47.75 37.75 26 24.5 61.75,
S #3 41.5 53 25.5 -54.5 50.75 37 26.5 19.25 63.5:S #9 40.5: 53.5 26 -53 51.5 37 25: 18.5 33.75I
E #5 41 59 24.5 -63.5 33-15 31.25 26 21 35,.,C #6 41.5 59.5 24 -63.25 38 6 26 19.5 35.25
E #2 39 1 1.5 -64.5 37.75 6.25 276 21: 35.5N: # 38.5:1 20.5: 1 -65: 39: 6.75 27: -3.5: 33:
D' i : -2:L 17~ 1?.5j-66.251 38.75 6. 27.5: -1.5 33.5:#3 -2.25 20.25 -8 -65.5; 39 .7 27 -3 33
P #7 -2 20 -7 -66 40.5 6.5 7.5 -3 32.75:
A #9 -2 19.5 -8 -65.5 9.5: 5.5 7.5: -5.5 -10.5
5.I. I ..I. .I
Z %301
• "' %
.% " "w" % - % " ". . . . =- , w- , , , "~ w , v, W',W , - ~w 'a' w-,rp ,• ' 'e 4' '' "',° K ", .€ .' ", ' ' K.." ., *
w .w %
xyn - u. L ,w ,.,-; -
-/i6" F LATEOut of plane deflection at the center of panel i. referenced to the1,.mnitudinal straight line connecting "he mid p-,ints o.f that panel's .-transverse stiffeners.. See Fioue 3-2 for the definition o'f D(MAX)iL. ": '.
dp
',PANEL ,, , , " -"
' HEATED$ D( MAX )I L D( MAX )2L;11( MAX )3L:' D( MAX )4L: [ ( MAX )5L:;1( MAX )6L;' D( MAX )TL;D( MAX )SL]D( MAX RgL ]------- -------- - ........
F WELD 56 61 47 70.5 58.5 47 54 31 56 ' r . ,.'.-#5 62.5 93 45 66 32.5 40.5 56 54 59.5.'.
R 1 #4 62 85.75 43.5 -6 46.5 40 57.5 49.5 5 ,v"# 4 5. 25 -. 27 15 5 47 2 _?w
T #8 54.75 51 43.5 -8.75 61.25 43.5 48 2.25 53 .. ...#6 52.5 58.5 46.5 -6 56.25 53 1 48 8.75 54.5...-.,.'
P #1 50.75 55.25 49.5 -16.25 62.25 55.75 : 46.5 7.25 52.5 .-..-.A #7 51 55.5 1 49 -14.5 1 62 55.25 31.5 : 9 52.5 .. .,S #3 51.5 55.25 35 -12.75 64.5 53 32.25 10 54.5 .,::",.,S #? 51 i 57 35 -11.5 66 51.75 32 9 31.75 ., *' "
S , .. '- ..j
E #5 52 161.75 33.5 -19 50.25 46.75 33.5 110.75 34.5 %",.wC #6 52.5 62 32 -9 55 23.5 337 1 30 N2 51 22.5 1 28 -19.5 55.05 24 34 10.5 33.5N #8 51 23 27.75 -21 55.5 24 34 -13.5 31.75D #1 10.5 20 28.5 -22 55.5 24 34.5 1-11.5 31.5 " .4
#3 I 0 243 -,)1 56 22.5 34.5 -13 31.5 -... .P #7 9.25 22.5 2.25 -22.5 56.5 22.5 1S -13 31.25 -,,.,"%_
A # 1.5 23 2 1-20.5 56.5 . 4 -16.5 -11.35..%,•.. ,
%"% .]Z
%"w % ,'.
tasee r ei.32 f t.L
,PA,,L.,,:-,,,,/:HEATD* D IIA)1LD(IAX 2L0(AX )3:D(~X 4LD(~A )SL;( ,,"L:DAx.7L0,.A8LDX'9L
I I I.I ,-
I
APPENDIX W . ',
1/8" STIFFENED PLATE MID-PANEL DEFLECTION DATAD(MAX)iT AND D(MAX)iL
4'
This appendix contains the mid-panel deflection data.D(MAX)iT and D(MAX)iL. for the 1/8" stiffened plate. The datais in tabular form. All deflection readings are inthousandths of an inch. See Figure 3-2 for the definition ofD(MAX)ET and D(MAX)iL.
.r We,
- .--.. '..
V%
. I
3," -
-5 .. o.
303 ""L.'","
".." ,3".
1,8 PLAT E %,-,-',out ,of pl.ine de{'le-_tl',n 0t th,- ,,nent-,, pDa el , r fErer,,e#l I.: ther, , -- ,tra n)sverse s tl'aloht l ine .c.o, e ct in g the mi d' v,,Its -,f t h'at Da nli-I' #
,Innqltudinal stif'feierc. See Fzcur~e 3-2 fo:r the ,lfnt,:-, 1:f :, M .:. -
';E T D A ,T. 'MAX )'TDl( MAX)3T;11(MAY )4TI[lb MAX ) T;DIk AY ,61, . T11 lA .,T r . ti ioTj' AY , 'Z',
F WELD 69.5 7.5j 32.5 34.25 69,75 2:7.5 J; 7 4. _
1 #5 75.5 4 37 24 24.5 13 93.5 161 c3..."'',Z'.# 4 93 4.05 34 20.5 25 12 9S55 16 J 545'-'-.__-.
S #6 94 4 '19. r 2 26.5 13 96 , 1 J 6T #2 96.5 1 -5.5 43.5 20 287 4.25 9.25.. 75- 5 5 .'-S
#8 96 -6.5 43 110.5 28.. 15, 11.5 89 -1 54.5P #3 93.5 -8 -6 19.75 32.25 1 11 88 -1 J4
r,.;-A #1 126.5 -17.5 -6.5 14.75 40.75 7.5 90 -13 51.5 '--%,
S 7 175 -18 -7 16.5 47.75 1. 123 -"2-." -
S #9 127.5 -18 -5 .5 16.25 52 .5 4.5 122 7-2. 5 40 ml
E #5 129.5 -20 -6.5 20.25 -2 -4 PLATE WAS :DAM AGED -"'-""
0 AFTER 1"'-'
N DAMIAGE .",'..
D 5 107 1 1. 75 -52 -3 124.25 -16.5 -73.51 # 4 1 2 9 .2 5 1 -2 0 .5 1 - -1 .5 4 6 5 -4 .2 5 : .3 -1 5 -5 -7 .7P #1 108 -20.5 -9 -9.5 -JO -2.5 124 -16 -74.5 ,-,--, .i,#A #7 108 -1 .5 -9.25 -9.5 -52.5 -3 114 -15.5 -74.5s
3 %i
#1 67-25 -23 -8.5 -9.5 -55.5 -1.25 113.75 -15.75 -74 ''..''
P #17 67.25 -23 -8 -8 -58 -1.75 93.5 -13x -74.5--A --
s. -
1 #7 -8.5 -59 67.75 -11.75 """ .P #1 24.5 -23 -8.75 -59.5 ,"..",'
101 THE PLATE WAS DAMAGED WHILE TAKING OUT-OF-PLANE DISTORTION READINGS AF TER "
PANEL #5 WAS HEATED. FPANELS #19 AND #4 WERE AFFECTED -,..,-,
304 "" --
1/8" FLATE
Out f plane deflet:,r, 2t the center cf panel I. refereced tc: thel:noitudinal stralQht ine :,nne,-tiQ the Mil points :f that pane l stransverse stiffeners. See Fmoi'e 3-2 f.' the def~rt,:n *:i D MAX iL. -
PANEL;
HEATED* D( MAX lL:D MAY )2L; D( MAX )7L, D( MAX 1L!I1 MAY )5L! DiAX ML j7: M 7L P10, )X8L P M x )QL:
F WELD 48.75 -14 16 14.5 45.5 1:.5' 68.5 -8. : 17
I #5 55; -17 21 6 2.5 0 77.5 -C0; 41"R #4 74.75 -16.5 18.75 6.25 4 0.5 78.75 -10.5 42"S #6 76 -17.5: 24.5 6.5 6.25 3.5 78.5 -10.75 45;T N! 78 -27:28.25: 6.5 8 3.75 79.25 -10 43.75-
#8 79.25 -26.75 28.25 6.25 8.25 3.25 73 -37.5 43P #3 76.5 -27.75 -18.25 6 12 .5 0.75 71.75 -38 4.,5 7cA #1 118.5 -35.5 -19.25 0 21 3 74.5 -38.5 40.75;S #7 119.5 -35.75 -19 0.25 28.75 -2 113.75 -49.5 43.5S #9 120 -35.25 -18 -0.25 34 -7.5 113.75 -54 32.21.
E #5 121.5 -38.5 -18.5 3.5 -71.5 2-16 PLATE WAS DAMAGED .. ,.
c0 AFTER .''.,",,%
N DAMAG E"-".- .,,,D N5 122.5 -37 -22.75 1.75 -71 -14.75 115.25 -38.5 -82V "w. #''
# 12lt -38.5 -1.5 -25 -65.5 1 -17 114 -37.5 -83.5:LAE. AS.AADP # 101.5 -37.5 -22.25 -24 -68.75 -15.25 114.5 -38.25 -84 '
A #7 100.25 -37 -22 -24.-5 -71 -15 105 -37 -83.25 %-% '4%
..,. '
D % .. .- - ,.',_
#1 60.75 -40 -21 -24 -74.25 -14 105 -37.5 -83.25 , ,.,,,
P #7 59.75 -40.5 -21 -22 -76 -13.75 85.5 -33.5 -82.75A i; j
S6S 1 1 -3 --23.'.5.-7-
HS,,
305. % %
s '.,:%
lI TEPLT A DAA IL TAING OU-F-LN ITRIN REDIG AFE ..2 .PAE # ASHATD PANLSI AN #4 WER AFECE I I"- v"
I I2 I II 22 % .' ' I lI 2 I " , II I"2.2.2 ,
305 " " "" "~
.7 I "o,,,. .," %
APPENDIX X
AFFECT ON D(MAX)iT AND D(MIAX)iL OF LINE HEATINGEACH PANEL ON THE 3/16" STIFFENED PLATE
% e
There are two types of comparisons made in this appendix:1. the affect on D(MAX)iT and D(MAX)iL of line heatinq
each of the panels, and2the affect on D(MAX) of all other panels when line
heating just one panel.
All data in the tables are in thousandths on an inch.
-0 _J'
%- -
306' P#
. 3./16" STIFFENED PLATE. FIRST FPAS
PANEL N1
1. The affect ,:,n D(MAX)UT and D( MAX)1L :, line heatig 111 other
pane I s.
-14.5 -13 1 -1.75 -8 0.5
-3.75 8.25 -1 -0.5 6.5 -2.25
1 0 -i 0.2j 0.75 -0.5
2. The affe ct cn D( MAX) :,f all cther panels by heating panel #1
TRANSVERSE LONGITUD INAL
-14.5 -8 0.5 -1.75 ;-3.25 3
-3 3 0 -10.3 62.75
-1 0 -0.75 -1.5 -1.5 -2
- --- - - -- - - -- - - -- - - -- - - ----- - -- - -- - -
PANEL #2
1. The affect 0an D( MAX )2T and D( MAX )2L ':,f line heatino all :therpanels.
TRANSVERSE LONGITUDINAL
a 8 -26 -2 a -3.2- -32.3 -0.25a : - 32.3 a ,-O.
:-8.25 33.3 2.5 -7. 5 32 7.5a _____ a ___
0 2 0.5 0.25 -2.5 1.75
2. The affe t ':'n D( MAX ) :,f all ,:threr panels bv heatino panel #2
TRANSVERSE LONGITUDINAL
-13 -26 -9 -8 :-32.3 -'a. ..a . a ai
0.75 10.5 2.75 -0.5 6.25 1.5 1
-0.5 -4 a 2 0.5 -4.75
307
FANEL # 3 Jo
%
1 The affect on [( MAX )3T and I( MAX )3L of line heatino all ,ther %panels. %
TRANSVERSE LONGITUDINAL
0. _ I . 5 3__--1__14
0.5 - -21.5 3 -14
-0. -3 .I . I -.5.
-05I2 .5~A -0. -2 3 "'
The .ff--:,-t on] D(MAXU o-f all o-ther panels by heatino pantel #3 ,.m..
TRANSVERSE LONGITUDINAL
1 -2 :-21.5 0.5 :-0.25 -14 -- ". . .
I~~~~~~#.. .. 21 -.5 .5 2.5 2.20.5 0.75 1.7c 0.75 1
PANEL #4• .""
1. The affect in] [I( MAX 4T and Ni MAX )4L ,of line heatino all o:ther ' . "#,Panels.__ -
TRANSVERSE LONGITUDIAL "....
-3 0.75 1.25 :-10.3 -0.5 1.75 [lill J
.... .%-'. " % Y
-102 -12 .3 5-72 -4.5 2 .75 ,c.i.
-1.75 :-0.75 1 .5 1.75 :-2.25 1.25 .,, , ,,,
2. The affect :,n ,(MAX) .,f all other panels bv heating panel #4
TRANSVERSE LONGITUDINAL -
-3.75 -8.5 -0.5 -0.5 -7.25 -1.5 -
-io
-12 32 -1.75 1-72 14J -0.5
-0 -5.5 -6 1.5 -14.5 2-6.,
I I ill I I I II s
oa ', .- ..., .
3ANEL 084
1.Th afetcmt' MX)4 ad I MX 4Lcflnehetioal che
I %
% %a, , DL4% %. %
FANE.L 45
I The fe,-t ,:, 1' hAX .T ;-d [.MAY 5"L of line h-,Rtino all 1other %
TRANSVERSE LONGITUDINAL
3 ) ,95 -1 216
,',-, , . . -C. '-.I< -3 .-"= ".8 s 1 14 ' -26 ' -5 *
-!7- 5 115 O xI-0.25 8.5 1.I I I I r.
- - - - - - - - - - - - -
-. The afefect cn D( MAY. ,-,f all -,ther panels by heatino panel #5 %%%
TRANSVERSE LONGITUDINAL "
C ----- I ... .
8 25 3 3 .2- -3 32,I , .. I __ _I -3 _..5_, - I -* ,. . --. . .
. . . .. I .. . .. . . . . ." °S " " " °
:-12.3 :-29.8 :-11.5 -4.5 -26 -6.5t t . . . . . . . . . . . . . . . . . • , ".I " "'+
3.5 23 3.5 ' 23 3.% VI,' I . . . . I t"A W R~
.5 - .", . -I'% .
PANEL #6
1. The aff ect on D( MAX )6T and Di( MAX )6L --If line heatino all )t-herpanels. i •
TRANSVERSE LONGITUDINAL .....II I. .,. a . .,..: :
.. .. ' I . . .- ',... .,"-"-0 2.75 -0.75 2.75 1 . 2)., .
• .. , -. , I
1.75 -11.5 -1.5 -0.5 -6.5 t 9.5
-0.75 -6.5 0 i -0.5 2 -1.25
, -... . . -, J __" __,.__
2. The affect con EI(MAX) cf all other panels bv heating panel #6
TRANSVERSE LONGITUDINAL
-1 2.5 3.25 -'2.25 7.5 3.... . _ _ -I° "" - '. . '
9. %
,-12 -1.5 2,75 -
-0.5 2 -5.5 0 6.5 1.5 ,
309. ,..:.. . .30 ~~~.. . -""
SI•
* _------!
'..." .% P...'.
% %
%w % .1
PANEL 6 J i%
1. The affect on (MAX )7T and D, A 7L ,AX f line heat ino sill :-thePanels.
TRANSVERSE LONGITUDINAL... ..I .. .. .. ..•0
-1 -0.5 0.5 -1.5 0.5 0.75
-1 3.5 -0.5 1.5 2 ." II "' 1.c",.
1 -w' -
, .. . .. ,.. .V ..4J .-22 -13 -1.5 -5 , -0 - . 5. .. ..
_ _ _ , ..... . • • .. ..
V".% ." V .V,.-V
2. The affect in D(MAX) ,of .11 other panels bv heatino panel #7 %.."%% % %, %
, W. %TRANSVERSE LONGITUDINAL
1 0 -0.5 0.25 0.25 -0.5 - .....III I I II~
til 1 I i
;-1.75 :-1.75 :-0.75 1.75 -0.25 -0.5
-22 :i-1.75 1 -15 1.75 0 , - -* .. ......." " ' I • I
I I I I I I Ill I "II II
PANEL #8
1. The affect o:n D( MAX )8T and D(MAX)8L o--f line heatino all o:ther -Panels. *
TRANSVERSE LONGITUDINAL , V %r V, v
0 -4 0.75 -1.5 '-4.75 i
-5.5 23 2 -4.5 2 3 6.5 %..... ,I I ••
:-1.75 :-41.5 :-5.25 1.75 :-42.5 -I
S"b% %'% . l
2. The affect on EI(MAX) of all other panels bv heatinQ panel #8 %
TRANSVERSE LONGITUDINAL * '-
0 -2 1.25 0.75 -2.5 1
-0.75 11.5 -6.5 :-2.25 QC 2
-13 -41.5 1 -10 :-42.5 1 t-r 9 i
310 '....... ,. ..... , . .... , -S...'...'. .* . '
Wt. % .% .%.. . . i C .]
t31 02 ""-"""'""-tc't.t at ut ~d J~L.P & . A..P, "' '-. .. -.
- - - - Pr. T °r'rd- .,wr - -
PAN'E L 49 I . |
T R AN SV ERSE L ON I T UD I N AL ,
I t I
0 75- 1.7c 2-
3.5 -55.5 ."'
' : A.'
.1. a%. 9 .8
The affect on D( MAX f 11 other p ne s by heatino pael er#9
TRANSVERSE LONGITUDINAL
,,,,,, _ J_
-1 0.5 0. -0.5 I 1.75 0 --.
1.5 0.75 0 1.25 1.5 :-I 25
-1.5 .-5 0-29.8 -0.25 -1 ,_ 18, , , % % a a
_ _- --- - - - - .- - -. ._-- -
0025 3,,.'. -.
..,, -,. ,' . ,
%". \."%" '..%
- °"'N o" '
"v'v .%." % " ,
4?-"•"' .- %
.'- ." '. " - %
311 . o] .'a'- t-7_ .- )
"- 0 0 %%,'
' ;,.' ."_-,, 1, , .' .' ' ",. ," _-_" , .' .'.% .%.%'.' .----'-------------------------",-"-------"---'-.----"------""---"--- """" .
.
~~..wwwuwwmi~~wwuwv Uwv W WWu'W7 YV, 3V,~ .1k 77.7-~ '~ ~V
_% N
B. 3/16" STIFFENED PLATE. SECOND PASS
'ANEL 01 0 .0
1. The Rffe,-t on D( MAX )1T .nd D(MAX )I of line heatino all other-
panels.TRANSVERSE LONGITUDINAL
-40.5 -2.5 0.25 -40.5 -1.5 -0.5 %
N/A -0.5 0. NIA 0.5 10.5-
'- I .% , .. %-0.25 -0.5 0 !-0.75 0 1.25 . -_ _ ,,-_
2. The affect :,n D( MAX) ,: all -,,ther panels by heating panel 41 .-'"...
TRANSVERSE LONGITUDINAL -......_-_- I ____ 3 I
-40.5 -3.5 0.5 :-40.5 -3 1 0.75 % %
:-1.25 -0.25 -0.25 -1 0 0__--_i_. . . . . . i _. . . . .
0.5 2 O.5 :0.5: 2 :-0.25"
PANEL #2 .
1. The affect ':'n D( MAX )2T and D( MAX )2L ,-,f line heatino all otherpanels.
TRANSVERSE LONG ITUDINAL
-3.5 :-39.5 3.25 -3 :-39.5 : 3 :
N/A : 6 0.5 NIA : 5.75 : 0.25 :
-0.25 ', 0.5 -0.5 -0.5 ', 0.5 ', 0.5.,_. .. .. . .,
2. The affect on D(MAX) of, all o:ther panels by heatino panel #2""2'%"'"x'
TRANSVERSE LONG ITUD INAL Nk.¢ .' ''
-2.5 ;-39.5 -5.5 -1.5 -39.5 -4 %J?-
.... ,...-,. *v*,**.4,.*."
-1.25 :-0.25 0.25 -0.5 0.5 0.5 ''. .,, ',r
-- I - I. . .. 3 _ _ Ii3
, - - - - , . . . . . . . . . .
1 1.5 0.25 0.25 -0.. -
3 2 . . _
TRANVERS LOGITUIN1I, u " " " " " - " " ' " " " " , - .
°" " "' • " ' " " " " " " "-- " . " . " . " . "
PANEL #3
1. The affect ,,n D( MAX )3T and D( MAX )3L of line heptlno al1 otheF
panels.TRANSVERSE LONGITUDINAL
0.5 -5.5 -27.5 0.75 -4 -26.5
N/A -2.5 -0.5 N/A -2.5 -1.50.5 - I O. I
1 0.5 -1 0.25 -0.25 :-0.25...... ___ I ...... __ i___
2. The affect ,:-n D( MAX ) of all other panels by heatino panel #3
TRANSVERSE LONGITUDINAL. . . . . I . . . . . . . I I . . .
-0.25 3.25 :-27.5 -0.5 3 ,-26.5
0.75 0.25 :-0.75 1 0.5 -1.5
-0.5 -1.5 0.5 0 -1.5 0
PANEL #4
1. The affect on D(M4X)4T and D(M4L of of line heating all otherpanels.
TRANSVERSE LONGITUDINAL* ______ II II ______
-1.25 -1.25 0.75 -1 -0.5 1
N/A -8 0.25 N/A -5.5 0
-0.5 -0.5 0.5 -1.5 -1.5 2I II . . . . . .I
2. The affect o:n D(MAX) of all other panels by heating panel #4
TRANSVERSE LONGITUDINAL
y r
i . . . . i _ _ _
,I.. . . . . I .. . . . .
W'
" "' " " #" °' ' "
* I ' IP#' r I I' I'"' . 'z , ' ', ,''' . ' ", '- ,m . '- . '-' '- . , ' .
" '-
PANEL #5
1. The aff ect o:n D( MAX )5T and D( MAX )5L of line heating all otherpanels.
TRANSVERSE LONGITUDINAL
-0.25 '-0.25 0.25 0 0.5 0.5
N/A -18.3 4.75 N/A -15.8 4.75
1.5 1.25 -1 0.5 0 0
2. The affect oan D(MAX) -:f all other panels by heating panel #5
TRANSVERSE LONGITUDINAL
-0.5 6 -2.5 0.5 5.75 -2.5
-8 :-18.3 -5.5 -5.5 -15.8 -4
0.5 0.25 0.5 1.75 1.75 1.25
PANEL #6
1. The affect :,n D(MAX)6T and D(MAX)6L caf line heatinQ all otherpanels.
TRANSVERSE LONGITUDINAL
:-0.25 0.25 -0.75 0 0.5 -1.5
NA -5.5 1-25.5 NA -4 :-23.3
a . . . . a
1 N/A aN/Aa'C C I 7
0.75 10.5 -1 a 0 0 0
0.25 4.75 :-25.3 0 4.75 ;-23.3
.. . .. I a.. .a .. .a
0 -1.5 0.25 0.25 0.25 -0.5
aai a- a I. I% %
.... -15 02.2 .5 -.
* ________ a"•"':' '. ". -'-' , "." -.-.- - " a a."" a'. "--"___ I''' a..:- ._-w_ _- _- * -: . .
FANEL #7
1. The affect on D( MAX )7T and D( MAX )7L of line heatino all otherpanels.
TRANSVERSE LONGITUDINAL. . .. . . I . . . . I . . . . I . . .
0.5 1 -0.5 0.5 0.25 0. . . . . . I I . . . . . . . I . . . . I . . . I . . . .
N/A 0.5 0 N/A 1.75 : 0.25III . . . . I . . . . . .
-19.5 0 0 -19.5 0 -1, - .. . I . . . . I . . . . .. . . . I I
2. The affect on D(MAX) of all other panels by heating panel #7
TRANSVERSE LONGITUDINALI I I . . . .
0.25 :-0.25 1 :-0.75 -0.5 0.25
: -0.5 1 1.5 0.75 -1.5 0.5 1 C
I ... .. .. I......
:-19.5 0 -0.25 :-19.5 1 0 1-0.25-- -- -- - - I ......... ... I ... ... I ..... .
PANEL #8
1. The affect on D(MAX)8T and D(MAX)BL of line heating all otherpanels.
TRANSVERSE LONGITUDINAL- - I . . . . . I . . . .
2 1.5 1 -1.5 2 1 -0.5 -1.5III I I I
N/A 2.5 -1.5 N/A : 1.75 0.25. . . . . . . . . I.. . .. . . I . . . .
0 -24.5 1 -2.5 0 -24 -3.5I . . . . . . . .I. . .
2. The affect on D(MAX) of all other panels by heating panel #8
TRANSVERSE LONGITUDINAL
-0.5 0.5 0.5 I 0 0.5 -0.25
-0.5 1 1.25 1 0.5 1 -1.5 0 0. . . . . . . I . . . . . .I I
1 0 :-24.5 : -2.5 0 -24 1-1.75
. . . . . . . . . .. I .
31
PANEL #9
1. The affe-t o'n 1( MAX )9T and EI(MAX)9L of line heatino all otherpanels.
TRANSVERSE LONGITUDINAL,, . . . . . . ,, I . . . .
0.5 0.25 -0.5 -0.25 -0.5 0
N/A 0.5 0.25 N/A 1.25 -0.5III - - I,
,-0.25 -2.5 -43.3 :-0.25 :-1.75 -42.6I .. . . . . ', . . . . . . '
2. The affect on D(MAX) of all other panels by heating panel #9
TRANSVERSE LONGITUDINALI I II . . . . I . . . . . . .
0 1 -0.5 -1 1.25 0.5 ,-0.25. . . . . I . . . . I . . . . , . . . . . . I . . . . I . . . .
I 0.5 -0.5 I I 20 I
I . . . . I . . . I . . . . I. .I . . . . I . . . .
0 1 -2.5 1-43.8 : -1 -3.5 1-42.6I I . . . . .._ I . . . . . .
316
APPENDIX Y
AFFECT ON D(MAX)iT AND D(MAX)iL OF LINE HEATINGEACH PANEL ON THE 1/8" STIFFENED PLATE
There are two types of comparisons made in this appendix:1. the affect on D(MAX)iT and D(MAX)iL of line heating
each of the panels, and2. the affect on D(MAX) of all other panels when line
heating just one panel.
All data in the tables are in thousandths on an inch.
317
. 1/8" STIFFENED FLATE. FIRST PASS
PANEL #1
1. The affect on D(MAX)IT and D( MAX )1L of line heatno R11 .otherpanels.
TRANSVERSE LONGITUDINAL
33 2.5 -2.5 4: 2-2.75
17.5 6 :19.75 6.25 1.25
0 -0.5 0 1 1.25 0.5
2. The affect on D(MAX) of all ,cther panels by heating panel #1
TRANSVERSE LONGITUDINAL
33 -9.5 -0.5 42 ,-7.75 -1
-5 8.5 -3.5 -6 8.5 2.2
2 -1 -2.5 2.75 -0.5 -2. . . . . . . . . . ..-- - - -. . . ..-- - -. . . . .
PANEL #2
1. The affect on D(MAX)2T and D(MAX)2L oaf line heatinq all otherpanels.
TRANSVERSE LONGITUDINAL
-9.5 9.5 -1.5 :-7.75 -9.5 -1
0.5 -3.5 -0.5 0.5 -3 -1
-0.5 -1 0 -0.25 0.25 0.5
2. The affect oin D(MAX) of all other panels by heating panel #2
fRANSYERSL LONGITUDINAL,,I . ..... ...... ,,.............
2.5 -9.5 4 2 -9.5 3.75III . . . . .. . . . .
0 2.25 1.25 0 1.75 0.25I I I . . . . . .I
-0.75 0.75 :-0.75 0.75 0.75 -1.25
318
PANEL #3
1. The affe.:t on D( MAX )3T and Dfl MAX )3L ,f line heatino al :1therpanels.
TRANSVERSE LONGITUDINAL
-0.5 4 -49 -1 3.75 ,-46.5
I ,.....-3 ', 4.5 5 .5 -2. 5 15.75
I . . . . I _ _-_
-0.5 -0.5 1.5 0.25 0 1
2. The affect en D(MAX) olf all other panels by heating panel #3
TRANSVERSE LONGITUDINAL
-2.5 -1.5 -49 -2.75 -1 -46.5
-0.75 3.75 -2.5 -0.25 4.25 -2.5
-1 0 -0.5 -1.25 -0.5 -0.25
PANEL #4
1. The affect on D(MAX)4T and D( MAX )4L ---f line heating all otherpane is.
TRANSVERSE LONGITUDINAL
-5 0 -0.75 -6 0 -0.25
-3.5, :-10.3 -0.5 0.25 -8.5 0.25
1.75 0.5 -0.25 0.25 -0.25 -0.5
2. The affect on D(MAX) of all other panels by heating panel #4
TRANSVERSE LONGITUDINALIIII . . . .. . . I.. .
18.5 0.5 -3 :19.75 0.5 :-2.25
-3.5 0.5 -1 0.25 1.5 0.5
2 0 i 1 1.25 -0.5 1 1
319
PANEL #5
1. The affe'ct c:,n D( MAX )5T and D(MAX)5L of line heating all other
panels.TRANSVERSE LONGITUDINAL
8.5 2.25 3.75 8.5 1.75 4.25
I I I . . . . . .I0.5 :-45.3 1.5 1.5 -43 2.25
7 :-0.25 4.75 7.75 0.25 5.25
2. The affect on D(MAX) of all other panels by heating panel #5
TRANSVERSE LONGITUDINALI I I.. . . . .
6 1 -3.5 4.5 6.25 -3 5
:-10.3 ,-45.3 :-14.5 -8.5 -43 -12.5
8.5 -1 1 4 9 1 -1.5 4
- -- - - - - - - - - - - - - - - - - - - - - - - - ------ _________
PANEL #6
1. The affect ,:n D(M6X)6T and D(M6L of o:f line heating all ,:,therpanels.
TRANSVERSE LONGITUDINAL... .. I.. . __..... . I I ', ___ _ _
-3.5 1 1.25 1 -2.5 1 1 2.25 0.25 1 -2.5
-1 :-14.5 1 0.5 :-12.5 1 3. .. . I.. . . I . . . .I.. . ___.. . . . .
: -0.75 1 -5 i -5 -0.5 -5.5
2. The affect ,on D(MAX) of all cother panels by heating panel #6
TRANSVERSE LONGITUDINAL 4
1 -0.5 5.5 1.25 1 '5.75 1
-0.5 1.5 1 1 0.25 2 -1 5 53. . . . . . . . . . .
0.5 1 -1 1.5 :-0.25 1-0.25 3
320
I~ u ~
PANEL #7
The affe:t ,, D(MAX)T and D(MAX 7 L of line heatino all .. ther- m . .,'
7T . " w" * W.%,
panels.TRANSVERSE LONGITUDINAL __
2 -0.75 -1 2.75 7 -1.25:II
.....
2 8.5 0.5 1 .25 9 :-0.25 W ""."
33 :-6.25 -1 :39.25 :-6.25 , 0%
The affect o:n D( MAX) :f all :ther panels by heatinQ panel #7.*
TRANSVERSE LONGITUDINAL %__ , * %..,.. "I -- I__I_
-- - --- . . . . . . . I. . . .. .. ' _.. .__.,____
1 -0.5 1 -0.5 1 -0.25 0.25 .,.,..,. - ..- . *,. ,.-. .- ,. , .
1.75 7 2 0.25 7.75 -5 ::.-.' -
* 33 :-13.5 3.5 :39.25 : -II 2.75 .,- . L'.--------------------- ' -....-- i-
PANEL #8 % ,
The af fect :n D( MAX )8T and D( MAX )8L --,f line heatinQ all :therpanels.
TRANSVERSE LONGITUDINAL
-1 : 0.75 : 0 -0.5 1 0.75 -0.5 .I I ...... I .,. .. .,:? =,.,.., .: .-_
- 0 : -1 -1 -0.5 : -1.5 :-0.25
:-13.5 :-27.8 : -6 -11 :-27.5 -4.5 %.%.....
The affect ,:n D(MAX) ,:f all other panels by heating panel #8 ,'?I" ''.I.-.". .. ,'IJ .
TRANSVERSE LONGITUDINAL " - • O-
.. . . *. . . I ... .... .. J . , .-0.5 : -1o. :-0.5 0 1 1.25 0.25 o:
-"-- - - - - I.II - * , 5'
10.5 1-0.25 :-0.75 : -0.25 :0.205 1 -0.5 %
:-6.25 1-27.8 :-0.75 -6.25 -27.5 -0.75
' _,.. .. - •• .,-...
321 . "
. ,, .. ..- ..5.
. - .P.
.'..NO .. ,
PANEL #9
1. The affect on E'(MAX )9T and D(MAX)9L 'f line heating all other
panels.TRANSVERSE LONGITUDINAL
-2.5 '-0.75 -0.5 -2 :-1.25 1 -2.5. . . . . I I, . . ..I
1 4 1.5 11 4 31
3.5 -0.75 -15 1 2.75 1-0.75 -11.3
2. The affect on D(MAX) of all other panels by heating panel #9
TRANSVERSE LONGITUDINAL
0 0 1.51 10.5 0.5 1
:-0.25 4.75 -s 0.5 5.25 -5.5
-1 -6 -15 1 0 -4.5 1-11.3
- - - - ---------------------------------------------
3
32
B. 1/8" STIFFENED PLATE. SECOND PASS
PANEL #1
1. The affect con D(MAX)IT and D(MAX)IL of line heating panels #5.#4. #1, and #7 a secoand pass.
TRANSVERSE LONGITUDINAL
2 .3 1-19.5
-1.5 3.25 -1.5 2.5
0 -1.25
2. The affe,-t ,.-n D(MAX) ,:f all other panels by heating panel #1
TRANSVERSE LONGITUDINAL
-21.3 0 0 1-19.5 1 :-0.75
0.75 -3.5 1.75 1 -3.25 1.75
1 :-0.75 :-0.75 0.5 -0.75 -0.5
PANEL #2
1. The affect on D(MAX)2T and D(MAX)2L cf line heating panels #5,#4. #1. and #7 a second pass.
TRANSVERSE LONGITUDINAL
0 '
-1.5 -I -1.5 -1.75
1 0.5
PANEL #3
1. The affect on D(MAX)3T and D(MAX)3L ,of line heating panels #5,#4, #1, and #7 a seond pass.
TRANSVERSE LONG ITUD INAL
0 ',1-0.75 '
1.5 -5 1.25 :-4.75
-0.25 0.25
323
a I a '%
PH EI a
1. The affect ,:n D( MAX )4T Fnd r1 MAX ),4L cf line he-tlno pRnels #5.#4, #1. and #7 a second pas.
TRANSVERSE LONGITUDINALII . . . . . . . . . . . .
0.75 1
:-27.8 1.25 -26.8 2
0 -0.25:. . .. I . . . .
2. The affect orn D(MAX) of all other panels by heating panel #4
TRANSVERSE LONGITUDINAL
-1.5 -1.5 , 1.5 -1.5 -1.5 1.25
-27.8 5.5 :-1.25 1 :-26.8 5.5 -2.25
-1.25 1.25 :-0.25 -1.25 1 -1.5
--------------------------------------------
PANEL #5
1. The affect o'n B(MAX)5T and D(MAX)5L of line heatinq panels #5.#4, #1, and #7 a sec:ond pass.
TRANSVERSE LONGITUDINAL. . . . I . . . . I . . . . I I . . . .
-4.5 325 I I. . . . . .. . . . .
5.5 -105 5.5 -1050. . . . . I . . . . I . . . . I . . . . . . . I . . . .
-2.5 I -2.25
2. The affect on D(MAX) cf all or-ther panels by heating panel #5
TRANSVERSE LONGITUDINAL
3.25 -1 -5 2.5 -1.75 1-4.75I .. . . I I',- . . ....
1.25 -105 -7.5 2 -105 :-7.25* . . . I I ', . . . . . .
2.25 16 -114 1.5 15.5 -114
324
PANEL #6
1. The affect c D( MAX 6T R)nd D( MAX )6L cf line heatiro panels 45,#4, #1. .and #47 _a secondl pass.
TRANSVERSE LONG ITUDINAL
1.75 1.75
-1.25 i-7.5 -2.25. . . . . .
-0.5 ' ,0.25
PANEL #7
1. The affect on D(MAX)7T and D(MAX)7L of line heating panels #5,#4, #1, and #7 a second pass.
TRANSVERSE LONGITUDINAL
i: I 0.5
'-1.25 2.25 :-1.25 1.5Ii . . . . . .
, -10 ',-9.5I . . . . . . i - I
2. The affect o:n D(MAX) :f all other panels by heating panel #7
TRANSVERSE LONGITUDINAL
0 1 1 i-0.25 -1.25 0.5 0.25
0 ' -2.5 , -0.5 1 -0.25 -2.25 0.25. . . . . . . I . . . . . .I
-10 : 0.5 , 0 -9.5 1.25 0.75
PANEL #8
1. The affect c, D(MAX)8T and D(MAX)8L of line heating panels #5,#4, #1, and #7 a secoind pass.
TRANSVERSL LONGITUDINAL
:-0.75 : ' -0.75I . . . . . . . . I.. .. .
1.25 :, 16 1 15.5I . . . . I . . . . . . . . . . .
0.5 1.25
III325
PANEL #t9
1.The af fect on 11( MAX '-9T and N' MAX )9L of linie heatillo Pal-e1l #54.#1. andL #7 a Sec:nd.) paSS.
TRANSVERSE LONGCITUDEINAL
-0.75 -0.5
:-0.25 -114 -1.5 114
0 £0.75
- -- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
326
C. 1/8" STIFFENED PLATE. THIRD PASS
PANEL #1
2. The affect cn D(MAX) ,f all ,:tler panels by heatino panel #1
TRANSVERSE LONGITUDINAL
-40.7 -3.5 0.75 -39.5 -3 1
0 -3 1.75 0.25 '-3.25 1
:-0.25 :-0.25 0.5 0 -0.5 0
PANEL #7
2. The affect ,:,Y D(MAX) of all cther panels by heatlng panel #7
TRANSVERSE LONGITUDINAL
-25 0 0.5 -1 -0.5 0
1.5 -2.5 -0.5 2 :-1.75 0.25
-20.3 2.75 1 -0.5 -19.5 4 0.5
327
ne!
. /8" STIFFENED PLATE. FOURTH PASS
PANEL #7
2. The affect on D(MAX) of panels #4. #5. #7. and #8 by heatinopanel #7.
TRANSVERSE LONGITUDINAL. . . . . .Ii . . . I . . . .
-0.5 -1 -1.5 -1.25
-25.8 1 1.25 -26 0.25. .. . I . . . . , . . . .. . . . I . . . .
---------------------------------------
PANEL #1
2. The affect on D(MAX) of panels #1, #2, #4, and #5 by heatingpanel #1.
TRANSVERSE LONGITUDINALI I . . . . . . . I . . . . . . I
-43 0 : 1-41.8 1.5 :
,-0.25 -0.5 '1 0 0.25SI ....... .
I I
328
i % .~ ' .rv
REFERENCES
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2. Pattee. H.E.. Evans. R.M.. Monroe. R., "FlameStraightening and its Effect on Base Metal Properties".Battelle Memorial Institute, Columbus. Ohio., SSC-198. August196?.
3. Holt. R.E.. "Flame Straightening Basics", Welding Journal.vol. 44, September 1965, pp. 49 - 52.
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10. Walsh, R.A., "Investigation of Distortion Removal inWelded Structures", S.M. Thesis, Department of OceanEngineering, M.I.T., Cambridge, MA., May 1969.
11. Duffy, D.K., "Distortion Removal in Structural Weldments",S.M. Thesis, Department of Ocean Engineering, M.I.T.,Cambridge, MA., May 1970.
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329
13. Taniguchi, C., "Out-Of-Plane Distortion Caused by FilletWelds in Aluminum", S. M. Thesis, Department of OceanEngineering, M.I.T., Cambridge, MA., September 1'57'2.
14. Henry, R.W.. "Reduction of Out-Of-Plane Distortion inFillet Welded High Strength Aluminum", S.M. Thesis, Departmentof Ocean Engineering, M.I.T., Cambridge, MA., May 1974.
15. Pattee, H.E.. Evans. R.M., Monroe, R.E., "ExperimentalFlame and Mechanical Straightening and its Effects on BaseMetal Properties", Battelle Memorial Institute, Project SR-185, Columbus, Ohio, July 1969.
16. Iwamura, Y., Rybicki, E.R., "A Transient Elastic-PlasticThermal Stress Analysis of Flame Forming", Transactions ofASME, vol. 95, February 1973, pp. 163 - 171.
17. Watanabe, M., Satoh, K., "Effect of Welding Conditions onthe Shrinkage Distortion in Welded Structures", WeldingResearch Supplement, August 1961, pp. 377 - 384.
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21. Papazoglou, V.J., Masubuchi, K., Goncalves, E., Imakita,A., "Residual Stresses Due to Welding: Computer-Aided Analysisof Their Formation and Consequences", SNAME, November 1982.
22. Agapakis, J.E., Papazoglou, V.J., Imakita, A., Masubuchi,K., "Study of Residual Stresses and Distortion in StructuralWeldments in High-Strength Steels", Final Report Preparedunder Contract N00014-75-0469, submitted to The Office ofNaval Research, November 1982.
23. Agapakis, T.E., Masubuchi, K., "Analytical Modeling ofThermal Stress Relieving in Stainless and High Strength SteelWeldments", Welding Research Supplement, June 1984, pp. 187 -196.
24. Tsai, C.L., "Modeling and Control of Out-Of-Plane WeldingDistortion in Fabricated Structure Members", Publisher anddate unknown.
330
25. Shin. D. B. , "Finite Element Analysis of Out-Of-PlaneDistortion of Welded Panel Structures", S.M. Thesis,Department of Ocean Engineering, M.I.T., Cambridge, MA.,May 1972.
26. Masubuchi, K., Imakita, A., Miyachi, H., Miyake, M.,"Development of an Intelligent System for Flame StraighteningPanel Structures", Paper to be Presented at The NationalShipbuilding Research Program, Ship Production Symposium,1987.
27. Ingerson, F.E.. Conversation on the welding sequence touse while welding the I/8" stiffened plate, Middlesex WeldingSupply, Cambridge, MA, January 1987.
28. Masubuchi, K., Terai, K., "Future Trends of Materials andWelding Technology for Marine Structures", SNAME, June 1976.
331
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