Mixing enhancement in compressible base flows via generation of streamwise vorticity

C. J. Bourdon, J. C. Dutton, C. J. Bourdon, J. C. Dutton

Research output: Contribution to journalArticlepeer-review

Abstract

The effects of adding streamwise vorticity to the boudary layer of an axisymmetric afterbody on the development of the near-wake region was demonstrated. The addition was done through the use of delta-shaped tabs mounted on the afterbody. The tabs generated streamwise vorticity persisted through the base corner expansion and into the near wake, increasing mixing and base drag. The streamwise structure was destablized by the reattachment process, and there was no trace of these structures in the end-view images.

Original languageEnglish (US)
Pages (from-to)1633-1635
Number of pages3
JournalAIAA journal
Volume39
Issue number8
DOIs
StatePublished - Aug 2001

ASJC Scopus subject areas

  • Aerospace Engineering

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