Linear and non-linear stability analysis of boundary layers over a hump by using PSEPSE 기법을 이용한 Hump 위 경계층의 선형 및 비선형 안정성 해석

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 858
  • Download : 0
Linear and non-linear stability analysis of incompressible and supersonic/hypersonic boundary layers over a two-dimensional smooth hump is carried out by using parabolized stability equations (PSE). A hump with a height smaller than the boundary layer thickness was considered. For incompressible boundary layer, overall destabilization influence of the hump is confirmed for both linear and non-linear evolution of instabil-ity waves. For linear stability, effects of several parameters including frequency, hump height, and wave obliqueness are examined. Comparisons of the linear PSE results with those from linear stability theory (LST) are also given. The discrepancy between the LST and linear PSE results mainly observed in the vicinity of the hump is found to be caused by both the flow non-parallelism and the transient behavior of PSE approach. The transient behavior sometimes accompanying wiggling in the growth rate curve is found to vary depending on the flow configurations such as frequency and hump height. Non-linear PSE analysis is carried out to examine non-linear evolution of Tollmien-Schlichting wave and subharmonic breakdown. Influence of frequency, hump height, and initial amplitude is investigated. The results demonstrate that disturbances can be amplified very much by the non-linear interaction due to the presence of hump in spite of very low level of disturbance amplitude, which suggests that the hump can bring forth earlier breakdown even for the case of rather small initial amplitude disturbances. Through analyses on subharmonic breakdown, it is found that the amplitude of primary wave affects most the growth of the secondary wave. Linear evolution of oblique first mode wave and oblique breakdown in Mach 1.6 boundary layer are analyzed for supersonic case. An overall effect of the hump on destabilization was similar to the case of subsonic boundary layer. For the case of linear stability, major difference was in the location where the largest dest...
Advisors
Park, Seung-Oresearcher박승오
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2013
Identifier
513985/325007  / 020085070
Language
eng
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2013.2, [ x, 118 p. ]

Keywords

Boundary layer; Linear stability; Non-linear stability; Hump; 경계층; 선형 안정성; 비선형 안정성; Hump; 포물형 안정성 방정식; Parabolized stability equations

URI
http://hdl.handle.net/10203/179614
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=513985&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0