지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2014.5
- 수록면
- 198 - 202 (5page)
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초록· 키워드
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The crossflow effect was considered on crossflow transition. The original γ-Re<SUB>θ</SUB> transition model was applicable 3 dimension transition analysis, but this transition model was not enough considering crossflow effect. In the present study, improved transition transport equation was developed for simulating 3 dimension crossflow transition phenomena in infinite swept wing configuration. The experimental data using infinite swept wing were used for comparison with numerical results for crossflow transitional flow. The infinite swept wing consisted of NLF(2)-0145 airfoil and 45° sweep angle. The swept wing was tested at ?4° angle of attack and Reynolds numbers from 1.92×10<SUP>6</SUP> to 3.73×10<SUP>6</SUP>. The measured transition locations compared remarkably well with computations using improved transition transport equation for all investigated flow cases.
목차
1. 서론
2. 수치해석 기법 및 해석 조건
3. 결과
4. 결론
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UCI(KEPA) : I410-ECN-0101-2015-420-001667031