참고문헌
- 신정우, 이상욱, 김태욱, 황인희, '4인승 선미익기 비행하중해석' 한국항공우주연구원 Technical Memo, KARl-AUG-TM-2005-013
- 심재열, 황인희, 류정주, '전기체 구조시험설비', 항공우주학회 춘계학술발표회 논문집, pp.47-50, 1999
- 김성찬, 김성준, 황인희, '전기체 구조시험의 피크 하중 해소방안 개발', 항공우주학회 춘계학술발표회 논문집, pp.422-425, 2004
한국군사과학기술학회지 (Journal of the Korea Institute of Military Science and Technology)
- 제9권4호
- /
- Pages.15-23
- /
- 2006
- /
- 1598-9127(pISSN)
- /
- 2636-0640(eISSN)
4인승 선미익 경항공기 전기체 정적 구조시험
Full Scale Airframe Static Test of 4 Seater Canard Airplane
-
신정우
(한국항공우주연구원)
;
-
김성찬
(한국항공우주연구원)
;
- 김성준 (한국항공우주연구원) ;
- 채동철 (한국항공우주연구원) ;
- 이상욱 (한국항공우주연구원) ;
-
김태욱
(한국항공우주연구원)
;
-
심재열
(한국항공우주연구원)
-
Shin, Jeong-Woo
(KARI)
;
-
Kim, Sung-Chan
(KARI)
;
- Kim, Sung-Jun (KARI) ;
- Chae, Dong-Chul (KARI) ;
- Lee, Sang-Wook (KARI) ;
-
Kim, Tae-Uk
(KARI)
;
-
Shim, Jae-Yeul
(KARI)
- 발행 : 2006.12.29
초록
In this paper, full-scale airframe static test of 4-seater canard airplane(the Firefly) was explained. From the results of the structural analysis, 5 design limit loads test conditions and 11 design ultimate loads test conditions were selected. Test loads analysis was performed and test fixtures and load control system(LCS) were prepared to realize the test loads. To protect the test article during the test, the overload protection system was prepared. Strain and deflection values were acquired through the data acquisition system(DAS) to verify the structural analysis results.
키워드