The present paper extends existing design formulae [Int. J. Solid Struct. 17 (1981) 827; J. Compos. Struct. 47 (1999) 737] for composite repairs to cracked metallic skins to include the bonded repair of rib stiffened wing skins. These design formulae are validated by comparison with the results of a series of 3D finite element studies and an experimental test program.
展开▼
机译：本文扩展了现有的设计公式[Int。 J.固体结构。 17（1981）827; J. Compos。结构。 47（1999）737]对破裂的金属蒙皮进行复合修复，包括对肋骨加硬的机翼蒙皮的粘结修复。通过与一系列3D有限元研究和实验测试程序的结果进行比较，可以验证这些设计公式。
展开▼
