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학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2005.3
- 수록면
- 80 - 86 (7page)
이용수
초록· 키워드
오류제보하기
In order to control the transonic flow field with a shock wave, a condensing flow was produced by an expansion of moist air on a circular bump model and shock waves were occurred in the supersonic parts of the fields. Furthermore, the additional passive technique of shock-boundary layer interaction using the porous wall with a cavity underneath was adopted in this flow field. The effects of these methods on the shock wave characteristics were investigated numerically. The result showed that the flow fields might be effectively controlled by the suitable combination between non-equilibrium condensation and the position of porous wall.
목차
ABSTRACT
1. INTRODUCTION
2. COMPUTATIONAL ANALYSIS
3. RESULTS AND DISCUSSIONS
4. CONCLUSIONS
REFERENCES
참고문헌 (11)
참고문헌 신청
[학술지(정기간행물)] - L / 1983 / Passive Shock Wave/Boundary Layer Control for Transonic Airfoil Drag Reduc-tion
[학술지(정기간행물)] - Prog. Aerospace Sci / 1988 / Passive Control of Shock-Boundary Layer Interaction 25 : 271 ~ 296
[학술지(정기간행물)] - T / 1997 / Effect of Nonequilibrium Homogeneous Condensation on Flow Fields in a Supersonic Nozzle Journal of Thermal Science 6 (2) : 90 ~ 96
[학술지(정기간행물)] - Matsuo / 1997 / Effect of Nonequilibrium Condensation of Moist Air on the Boundary Layer in a Supersonic Nozzle J. of Thermal Science 6 (4) : 260 ~ 272
[학술지(정기간행물)] - / 1975 / Condensation of Water Vapor with or without a Carrier Gas in a Shock Tube (201.)
[학술지(정기간행물)] - Prog. Aerospace Sci / 1988 / Passive Control of Shock-Boundary Layer Interaction 25 : 271 ~ 296
[학술지(정기간행물)] - T / 1997 / Effect of Nonequilibrium Homogeneous Condensation on Flow Fields in a Supersonic Nozzle Journal of Thermal Science 6 (2) : 90 ~ 96
[학술지(정기간행물)] - Matsuo / 1997 / Effect of Nonequilibrium Condensation of Moist Air on the Boundary Layer in a Supersonic Nozzle J. of Thermal Science 6 (4) : 260 ~ 272
[학술지(정기간행물)] - / 1975 / Condensation of Water Vapor with or without a Carrier Gas in a Shock Tube (201.)
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