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[2] Alten F. Grandt JR, "Fundamentals of Structural Integrity: Damage Tolerant Design and Nondestructive Evaluation," Wiley-Interscience, November 3, 2003.
[3] Jong-Heon Kim and Young-Sik Joo, "Case Study of F-15 Airframe Battle Damage Repair Design and Assessment Procedure," Journal of The Korean Society Aeronautical and Space Sciences, Vol. 37, No. 1, pp. 105–112, 2009.
[4] TO 1-1A-1. Engineering Handbook Series for Aircraft Repair, Para. 3.13., Fig. 3-13-19..
[5] TO 1F-5E-3. Structural Repair USAF Series F-5E/F Aircraft, Para 2.24.6.6, Page 2-185, Fig. 2-27..
[6] TO KS1F-16C-3-1. Structural Repair, ROKAF Series F-16C/D Aircraft Block 32 and 52, Para. 1.12.4, Table 1-12..
[7] MSC Nastran 2018. Linear Static Analysis User's Guide, MSC.Software..
[8] DK Oh. "MSC Nastran Nonlinear Analysis Application," MSC Software 2014 Korea Users Conference, pp. 1–21, 2014.
[9] MIL-HDBK-516C, DoD Handbook. Airworthiness Certification Criteria, pp. 8712 December, 2014.
[10] e-CFR(ecfr.gov). Limit and Ultimate Loads, Part 23, Sec.23.2230..
[11] NATO Standard, AEP-83. Light Unmanned Aircraft Systems Airworthiness Requirements, ER.1.1, UL 2.4..
[12] Tuan Nguyen. "Stress Around Bolt Hole Comparison Between a Closed Form Calculation Method and Finite Element Analysis," MSC Software 2013 Regional User Conference, pp. 1–20, 2013.