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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 1997.3
- 수록면
- 35 - 46 (12page)
이용수
초록· 키워드
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In this study comparison of experiment results with the computed results of linear theory and nonlinear theory using singularity method was obtainable. Specially singularity points like sources and vortexes on hydrofoil and freestreamline were distributed to analyze two dimensional flow field of supercavitating cascade using nonlinear theory, and governing equations of flow field were derived and hydraulic characteristics of cascade were calculated by numerical analysis of the governing equations.
The results compared linear theory and nonlinear theory with the experiment results of the study are as follows: The tolerances of nonlinear theory were larger than those of linear theory in case of α< 10˚.
Moreover the computational range of attack angles could be expanded from a = 10˚ to a=25˚, the flow field of supercavitating cascade could be analyzed in the condition which the wake thickness and the length of cavity are a variable.
The shapes of cavity were changed sensitively according to various variable such as attack angles, pitches and wake thickness, and the pressure distribution of hydrofoil surface was identical almost disregarding wake thickness but changed largely according to attack angle and the length of cavity. Lift coefficient and drag coefficient were reduced according to increasing of wake thickness but the influences of wake thickness were very little in the situation of small pitch and long cavity.
The results compared linear theory and nonlinear theory with the experiment results of the study are as follows: The tolerances of nonlinear theory were larger than those of linear theory in case of α< 10˚.
Moreover the computational range of attack angles could be expanded from a = 10˚ to a=25˚, the flow field of supercavitating cascade could be analyzed in the condition which the wake thickness and the length of cavity are a variable.
The shapes of cavity were changed sensitively according to various variable such as attack angles, pitches and wake thickness, and the pressure distribution of hydrofoil surface was identical almost disregarding wake thickness but changed largely according to attack angle and the length of cavity. Lift coefficient and drag coefficient were reduced according to increasing of wake thickness but the influences of wake thickness were very little in the situation of small pitch and long cavity.
목차
Abstract
1. 서론
2. 관련이론
3. 결과 및 고찰
4. 결론
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