TABLE 6-6. FIBERGLASS POLYESTER LAMINATES 



CRITICAL BUCKLING LOADS - POUNDS PER LINEAR INCH 



2 OZ. MAT - LOADED EDGES CLAMPED - 



REMAINING EDGES SIMPLY SUPPORTED 



PHYSICAL CONSTANTS: 

 E x = E Y = 0.86x10 6 PSI 

 Gxy = 0.40x10 6 PSI 

 0"xy = CTyx = 0.37 



THICJCNESS-H EQUALS 0,1250 INCHES 



6-yb 



