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.23 no.4, 2020년, pp.319 - 327
김덕주 (국방과학연구소 제3기술연구본부) , 하승룡 (국방과학연구소 제3기술연구본부) , 강민성 (한화시스템(주) 기반기술연구소) , 허재훈 (한화시스템(주) 기반기술연구소)
In this study a methodology to evaluate fatigue life of the electronic parts for the fighter radar unit under random vibration loading is presented. To do this, one parameter for the 3-σ RMS quation of Steinberg fatigue model is modified to come up with a printed circuit board(PCB) with multi...
* AI 자동 식별 결과로 적합하지 않은 문장이 있을 수 있으니, 이용에 유의하시기 바랍니다.
Dave S Steinberg, "Vibration Analysis for Electronic Equipment," John Wiley & Sons, Inc. USA, p. 42, pp. 215-224, p. 368, 2000.
Andres Garcia, Felix Sorribes-Palmer and Gustavo Alonso, "Application of Steinberg Vibration Fatigue Model for Structural Verification of Space Instruments," AIP Conference Proceedings 1922, 100003, 2018.
Hui Wei, and Liangjun Xu, "Research on Dynamic Model of Printed Circuit Board based on Finite Element Method," AIP Conference Proceedings 1864, 020082, 2017.
Bruno de Castro Braz, Flavio Luiz de Silva Bussamra, "An Enhanced Random Vibration and Fatigue Model for Printed Circuit Boards," Latin American Journal of Solids and Structures, pp. 2402-2422, 2017.
Steinberg & Associates, "Assessment of Vibration on Avionic Design," Prepared for Universal Energy System, Dayton, OH, August 1984.
M. D. Prashanth, "Vibration Analysis of Printed Circuit Boards: Effect of Boundary Condition," AIP Conference Proceedings 1943, 020018, 2018.
Deokjoo Kim and Seungryong Hah, "Preliminary Design Report of AESA Radar Unit(Mechanical Structure)," ADDR-501-192427, p. 5, pp. 15-16, 2019.
K. J. Bathe, "Finite Element Procedure in Engineering Analysis," Prentice-Hall, Inc., Englewood Cliffs, NJ07632, pp. 251-255, 1982.
MIL-HDBK-5J, "Metallic Materials and Elements for Aerospace Vehicle Structures," 31 January 2003.
Isola, "185HR Laminated and Prepreg Data Sheet," 31 January 2003.
Warren C. Young, "Roark's Formulas for Stress and Strain," McGraw-Hill Book Company, Newyork, p. 462, 1989.
Deokjoo Kim, Seungryong Hah and Jaeyoun Youn, "A Study on the Application Method of Steinberg Fatigue Limit Equation for Electronic Part Life Assessment of Fighter Aircraft Radar," ADDR-401-200730, 2020.
MIL-STD-810G, "Department of Defense Test Method Standard," Part Two, Method 514.6 & 519.6, 31 October 2018.
*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.