Numerical study of shock interactions on double-wedge geometries

Joseph Olejniczak, Michael J. Wright, Graham V. Candler

Research output: Contribution to conferencePaper

4 Scopus citations

Abstract

Steady shock interactions in perfect gas flows over double-wedge geometries are studied using computational fluid dynamics. In inviscid flow, four possible steady shock interactions are observed. These are the standard Type IV, V, and VI, as well as an apparent new interaction. In the Type IV and new interactions, a supersonic jet forms along the body surface. This jet produces oscillations in flow quantities on the surface. Preliminary laminar viscous calculations show that steady solutions exist for a range of Reynolds numbers and second wedge angles. These flows are very sensitive to the level of grid resolution, and it is only possible to correctly produce these interactions with very fine grids.

Original languageEnglish (US)
DOIs
StatePublished - Jan 1 1996
Event34th Aerospace Sciences Meeting and Exhibit, 1996 - Reno, United States
Duration: Jan 15 1996Jan 18 1996

Other

Other34th Aerospace Sciences Meeting and Exhibit, 1996
CountryUnited States
CityReno
Period1/15/961/18/96

Fingerprint Dive into the research topics of 'Numerical study of shock interactions on double-wedge geometries'. Together they form a unique fingerprint.

  • Cite this

    Olejniczak, J., Wright, M. J., & Candler, G. V. (1996). Numerical study of shock interactions on double-wedge geometries. Paper presented at 34th Aerospace Sciences Meeting and Exhibit, 1996, Reno, United States. https://doi.org/10.2514/6.1996-41