메뉴 건너뛰기
.. 내서재 .. 알림
소속 기관/학교 인증
인증하면 논문, 학술자료 등을  무료로 열람할 수 있어요.
한국대학교, 누리자동차, 시립도서관 등 나의 기관을 확인해보세요
(국내 대학 90% 이상 구독 중)
로그인 회원가입 고객센터 ENG
주제분류

추천
검색
질문

논문 기본 정보

자료유형
학술저널
저자정보
Hariharan Kallath (Rolls-Royce and Pusan National University Technology Centre in Thermal Management) Foster Kwame Kholi (Rolls-Royce and Pusan National University Technology Centre in Thermal Management) June Kee Min (Pusan National University)
저널정보
한국전산유체공학회 한국전산유체공학회지 한국전산유체공학회지 제26권 제4호
발행연도
2021.12
수록면
65 - 82 (18page)
DOI
10.6112/kscfe.2021.26.4.065

이용수

표지
📌
연구주제
📖
연구배경
🔬
연구방법
🏆
연구결과
AI에게 요청하기
추천
검색
질문

초록· 키워드

오류제보하기
The significance of low Reynolds flows increased due to the emergence of low speed flying vehicles. Therefore, the flow control methods deserve more attention. In the present study, the application of a differential temperature on the surfaces of a slotted double-element airfoil is numerically evaluated at a low Reynolds number turbulent flow condition. The main objective is to study the effects of differential temperature on the aerodynamics of the airfoil at various flap positions. Six flap positions were considered utilizing the overset meshing techniques after appropriate parameterization of the flap locations. The numerical results were validated against previous experimental results, and subsequently, the effects of the differential temperature on the aerodynamics of baseline and other configurations were clearly explained. The best configurations were identified with and without the presence of differential temperature. Moreover, it was found out that among all the considered configurations, a maximum of 4% increase in lift and 5% reduction in drag can be achieved through the application.

목차

1. Introduction
2. Computational Analysis
3. Results and Discussion
4. Conclusion
References

참고문헌 (44)

참고문헌 신청

함께 읽어보면 좋을 논문

논문 유사도에 따라 DBpia 가 추천하는 논문입니다. 함께 보면 좋을 연관 논문을 확인해보세요!

이 논문의 저자 정보

이 논문과 함께 이용한 논문

최근 본 자료

전체보기

댓글(0)

0

UCI(KEPA) : I410-ECN-0101-2022-559-000145075