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By Thoralf Skolem

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This process allows for the conventional orientation of fibers, that is, 0 deg (along the boom axis), 45 deg (bias), and 90 deg (circumferentially around the boom). The tailboom has a small taper to it as it transitions from the body of the helicopter to the tailrotor gearbox attachment. This taper presented a problem in dropping the plies. 24 in. (6 mm) wide, require a series of laps and gaps. A significant amount of effort was expended in trying to reduce the effect of the lap and gap by compacting the ply as it was laid on the tool; but these laps and gaps provide an inherent crack (or delamination) initiation source.

J. , Brandt, F.. , "Investigations of Delamination Criticality and the Transferability of Growth Criteria," Composite Structures, Vol. 36, No. 3/4, 1996, pp. 221-247. , Asp, L. , 'Assessment of Evaluation Methods for the Mixed Mode Bending Test," Journal of Composites Technology and Research, Vol. 21, No. 1, 1999, pp. 37-48. [34] Asp, L. , "'Effects of Moisture and Temperature on the Interlaminar Delamination Toughness of a Carbon/Epoxy Composite," Composites Science and Technology, Vol. 58, No.

5 in. 1 mm) in diameter. From the perspective of a global structural response, increasing the steel tup size (impactor diameter) from ~ in. 8 mm) to 2 in. 8 ram) showed very similar results relative to deflection and impact energy. However, locally within the structure there is a significant difference in maximum contact force between the tup diameters, influenced by the contact area between the tup and the specimen, as demonstrated by the tact that penetration never occurred with a 2-in. 8 ram) tup.

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