최소 단어 이상 선택하여야 합니다.
최대 10 단어까지만 선택 가능합니다.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기韓國軍事科學技術學會誌 = Journal of the KIMST, v.24 no.5, 2021년, pp.467 - 474
최동수 (공군사관학교 항공우주공학과)
A study on optimal shape selection of a mechanical fastening for the repair of crack defect of ROK Air Force F-5 fighter wing was conducted. The crack defect occurred in the spar of the wing, and the technical manual does not specify the repair method. However, ROK Air Force decided to develop a rep...
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.
Alten F. Grandt, JR. "Fundamentals of Structural Integrity : Damage Tolerant Design and Nondestructive Evaluation," Wiley-Interscience, November 3, 2003.
TO 1-1A-1, "Engineering Handbook Series for Aircraft Repair," Para. 3.13., Fig. 3-13~19.
TO 1F-5E-3, "Structural Repair USAF Series F-5E/F Aircraft," Para 2.24.6.6, Page 2-185, Fig. 2-27.
TO KS1F-16C-3-1, "Structural Repair, ROKAF Series F-16C/D Aircraft Block 32 and 52," Para. 1.12.4, Table 1-12.
MSC Nastran 2018, "Linear Static Analysis User's Guide," MSC.Software.
DK Oh, "MSC Nastran Nonlinear Analysis Application," MSC Software 2014 Korea Users Conference, pp. 1~21, 2014.
MIL-HDBK-516C, DoD Handbook, "Airworthiness Certification Criteria," Page 87, 12 December, 2014.
e-CFR(ecfr.gov), "Limit and Ultimate Loads," Part 23, Sec.23.2230.
NATO Standard, AEP-83, "Light Unmanned Aircraft Systems Airworthiness Requirements," ER.1.1, UL 2.4.
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.
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
오픈액세스 학술지에 출판된 논문
※ AI-Helper는 부적절한 답변을 할 수 있습니다.