TABLE 6-7. FIBERGLASS POLYESTER LAMINATES 



CRITICAL BUCKLING LOADS - POUNDS PER LINEAR INCH 



2 OZ. MAT - ALL EDGES CLAMPED 



PHYSICAL CONSTANTS: 

 E x = E Y = 0.86x10^ Ps | 

 Gxy = 0.40x10 6 PSI 



0"xy = Oyx = 0.37 



THICKNESS-H EQUALS 0.0625 INCHES 



LENGTH-S 



INCHES 



WIDTH-A 

 INCHES 



LENGTH-B 

 INCHES 



EQUALS 0.1250 INCHES 



LENGTH-B 

 INCHES 



WIDTH-A 

 INCHES 



LENGTH-B 

 INCHES 



495 312 251 224 209 



975 353 172 102 

 1046 375 160 105 



192 189 167 186 185 184 



428 278 191 155 136 126 119 115 112 



402 251 178 130 106 93 86 81 77 



385 229 166 124 94 78 69 63 59 



379 227 150 118 91 71 60 53 48 



368 217 145 107 88 70 56 48 42 



367 213 145 102 80 69 55 45 39 



377 210 139 101 76 63 55 45 37 



395 206 136 100 74 59 50 45 37 



420 207 137 9 6 74 57 46 41 37 



450 210 133 95 73 57 46 39 «« 



616 249 



667 263 141 



183 182 1B2 181 



107 106 105 105 



ieo 180 



179 179 



102 102 101 101 



6-100 



