NASA NTRS · 19860000058
Optimized Bolted Joint
Abstract
Computer technique aids joint optimization. Load-sharing between fasteners in multirow bolted composite joints computed by nonlinear-analysis computer program. Input to analysis was load-deflection data from 180 specimens tested as part of program to develop technology of structural joints for advanced transport aircraft. Bolt design optimization technique applicable to major joints in composite materials for primary and secondary structures and generally applicable for metal joints as well.
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Hart-Smith, L. J., Bunin, B. L., Watts, D. J.. 1986-06-01. Optimized Bolted Joint. https://ntrs.nasa.gov/citations/19860000058
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