DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | Chang, Keun-Shik | - |
dc.contributor.advisor | 장근식 | - |
dc.contributor.author | Kim, Jae-Soo | - |
dc.contributor.author | 김재수 | - |
dc.date.accessioned | 2011-12-12T07:16:24Z | - |
dc.date.available | 2011-12-12T07:16:24Z | - |
dc.date.issued | 1983 | - |
dc.identifier.uri | http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=63625&flag=dissertation | - |
dc.identifier.uri | http://hdl.handle.net/10203/26569 | - |
dc.description | 학위논문(석사) - 한국과학기술원 : 항공공학과, 1983.2, [ vii, 49 p. ] | - |
dc.description.abstract | Unsteady boundary layer equations are solved by a noniterative implicit numerical scheme which is second-order accurate both in time and space. The present numerical method provides initial data within the method itself by solving a reduced initial boundary value problem applicable at or very near the origin of a streamwise coordinate. The method has been applied to unsteady laminar boundary layers with large disturbance parameters such as transition to Falkner-Skan flow, oscillating Blasius flow, oscillating Stagnation-Point flow, constant accelerated flow and harmonically fluctuating boundary layer past a circular cylinder. The thermal effects are also considered in the boundary layers of the last application. Comparison with the existing data has demonstrated excellency of the present method both in accuracy and computer-time economy. | eng |
dc.language | eng | - |
dc.publisher | 한국과학기술원 | - |
dc.title | Numerical analysis of unsteady laminar boundary layers | - |
dc.title.alternative | 비정상 층류 경계층 유동의 수치해석 | - |
dc.type | Thesis(Master) | - |
dc.identifier.CNRN | 63625/325007 | - |
dc.description.department | 한국과학기술원 : 항공공학과, | - |
dc.identifier.uid | 000811060 | - |
dc.contributor.localauthor | Chang, Keun-Shik | - |
dc.contributor.localauthor | 장근식 | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.