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
- 학술저널
- 저자정보
- 발행연도
- 2014.6
- 수록면
- 8 - 16 (9page)
이용수
초록· 키워드
오류제보하기
Two-dimensional prediction capability of several analysis codes, such as XFOIL, MSES, and KFLOW, is compared and analyzed based on computational results of airfoil flows. To this end the transition transport equations are coupled with the Navier-Stokes equations for the prediction of the natural transition and the separation-induced transition. Experimental data of aerodynamic coefficients are used for comparison with numerical results for the transitional flows. Numerical predictions using the transition transport model show a good agreement with experimental data. Discrepancies have been found in the prediction of the pressure drag are mainly caused by the difference in the far-field circulation correction methods.
목차
1. 서론
2. 본론
3. 결과
4. 결론
References
참고문헌 (24)
참고문헌 신청
1. [보고서] - Granville, P.S. / 1953 / The Calculation of the Viscous Drag of Bodies of Revolution
2. [보고서] - Smith, A.M.O. / 1956 / Transition, Pressure Gradient and Stability Theory
3. [보고서] - van Ingen, J. / 1956 / A Suggested Semi-Empirical Method for the Calculation of the Boundary-Layer Region
4. [학술지(정기간행물)] - Drela, M. / 1986 / Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils / AIAA 1987 25 (10) : 1347 ~ 1355
5. [단행본] - Drela, M. / 1989 / Low Reynolds Number Aerodynamics / Springer-Verlag
2. [보고서] - Smith, A.M.O. / 1956 / Transition, Pressure Gradient and Stability Theory
3. [보고서] - van Ingen, J. / 1956 / A Suggested Semi-Empirical Method for the Calculation of the Boundary-Layer Region
4. [학술지(정기간행물)] - Drela, M. / 1986 / Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils / AIAA 1987 25 (10) : 1347 ~ 1355
5. [단행본] - Drela, M. / 1989 / Low Reynolds Number Aerodynamics / Springer-Verlag
이 논문의 저자 정보
이 논문과 함께 이용한 논문
최근 본 자료
댓글(0)
0
UCI(KEPA) : I410-ECN-0101-2015-420-001666352