Unsteady shock wave-vortex interactions in the compressible shear layer = 압축성 전단층에서의 이동 충격파-와동 상호 간섭 연구

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 363
  • Download : 0
Shock wave-vortex interaction in the compressible shear layers is investigated with both experimental and computational methods. Four different but related models are studied to broaden knowledge of the nonlinear shock wave dynamics. They are the interaction behind a finite wedge, a cone, a flat plate in short-term period, and a flat plate in long-term period. The investigated phenomena include such flow structures as shock-shock, shock-vortex, shock-vortexlet, and shock-slip layer interactions. The mechanisms of a few other type of secondary waves like the diverging acoustics and transmitted shock, not yet fully investigated by other researchers, have been explained. The three computational models for the shock-slip layer interaction have proved very informative for understanding of the complicated shock wave dynamics.
Advisors
Chang, Keun-Shikresearcher장근식researcher
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2000
Identifier
158037/325007 / 000965342
Language
eng
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2000.2, [ iv, 81 p. ]

Keywords

Shock wave; Holography; Compressible flow; 충격파; 와동; 전단층; 홀로그래피; 압축성 유동; Vortex; Shear layer

URI
http://hdl.handle.net/10203/26260
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=158037&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