1 |
National Academies Press, National Research Council, Division on Engineering and Physical Sciences, National Materials Advisory Board, Commission on Engineering and Technical Systems, Committee on Aging of U.S. Air Force Aircraft, "Aging of U.S. Air Force Aircraft : Final Report", October 30, 1997.
|
2 |
Jong-Heon Kim, 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.
DOI
|
3 |
TO 1-1A-1, "Engineering Handbook Series for Aircraft Repair," Para. 3.13., Fig. 3-13~19.
|
4 |
TO KS1F-16C-3-1, "Structural Repair, ROKAF Series F-16C/D Aircraft Block 32 and 52," Para. 1.12.4, Table 1-12.
|
5 |
MSC Nastran 2018, "Linear Static Analysis User's Guide," MSC.Software.
|
6 |
MIL-HDBK-516C, DoD Handbook, "Airworthiness Certification Criteria," Page 87, 12 December, 2014.
|
7 |
e-CFR(ecfr.gov), "Limit and Ultimate Loads," Part 23, Sec.23.2230.
|
8 |
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.
|
9 |
Alten F. Grandt, JR. "Fundamentals of Structural Integrity : Damage Tolerant Design and Nondestructive Evaluation," Wiley-Interscience, November 3, 2003.
|
10 |
TO 1F-5E-3, "Structural Repair USAF Series F-5E/F Aircraft," Para 2.24.6.6, Page 2-185, Fig. 2-27.
|
11 |
DK Oh, "MSC Nastran Nonlinear Analysis Application," MSC Software 2014 Korea Users Conference, pp. 1~21, 2014.
|
12 |
NATO Standard, AEP-83, "Light Unmanned Aircraft Systems Airworthiness Requirements," ER.1.1, UL 2.4.
|