- 고온 내열재료를 사용한 스마트 무인기 덕트의 열 구조 해석
- ㆍ 저자명
- 임종빈,윤동영,이근명,박정선,Im. J.B.,Yoon. D.Y.,Lee. K.M.,Park. J.S.
- ㆍ 간행물명
- 한국항공운항학회지
- ㆍ 권/호정보
- 2004년|12권 2호|pp.17-28 (12 pages)
- ㆍ 발행정보
- 한국항공운항학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
In unmanned aerial vehicle (UAV), the high temperature results from friction with the air, combustion of fuel and combustion gas of a nozzle etc. It causes serious problems in the UAV structure. The characteristic analysis of heat resistant metal and ceramic materials and creep analysis for the functionally graded material (FGM) is presented in this paper. FGM is composed of two constituent materials that are mixed up according to the specific volume fraction distribution in order to withstand high heat condition. In addition, the creep behavior of FGM applied in duct structure of an engine is analyzed.