1. Hart-Smith, L.J., 1976. Bolted joints in graphite-epoxy composites. NASA Contractor Report (NASA CR-144899). Long Beach, CA: Douglas Aircraft Company, McDonnell Douglas Corporation. Available at: https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19770008495.pdf.
2. McCarthy, M.A., 2001. BOJCAS: Bolted Joints in Composite Aircraft Structures. Air & Space Europe. Available at: http://www.smr.ch/bojcas/Reports/airspace-eu.pdf (accessed 01.02.10).
3. Mechanically-fastened joints for advanced composites – phenomenological considerations and simple analysis;Hart-Smith;Douglas Paper,1978
4. Stress analysis and strength prediction of mechanically fastened joints in FRP: A review;Camanho;Composites Part A: Applied Science and Manufacturing,1997
5. Characterization of bolted joint behaviour: MIL-HDBK-17 Accomplishments at Standardization;Shyprykevich;Journal of Composites Technology and Research, JCTRER,1995