Instability mechanisms in supersonic base flows

R. D. Sandberg, Hermann F Fasel

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

The hydrodynamic stability behavior of the near-wake is investigated using Direct Numerical Simulations (DNS) for a supersonic axisymmetric baseflow at M=2.46. As a consequence of the instability, coherent structures evolve that influence the mean flow behavior. Results are presented for two different Reynolds numbers, Re D = 30, 000 and Re D = 60,000. For these investigations, a high-order accurate compressible Navier-Stokes solver in cylindrical coordinates was developed. Simulations with various domain-sizes were performed to investigate the instability behavior to different azimuthal modes.

Original languageEnglish (US)
Title of host publicationAIAA Paper
Pages5803-5814
Number of pages12
StatePublished - 2004
Event42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States
Duration: Jan 5 2004Jan 8 2004

Other

Other42nd AIAA Aerospace Sciences Meeting and Exhibit
CountryUnited States
CityReno, NV
Period1/5/041/8/04

Fingerprint

Direct numerical simulation
Reynolds number
Hydrodynamics

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Sandberg, R. D., & Fasel, H. F. (2004). Instability mechanisms in supersonic base flows. In AIAA Paper (pp. 5803-5814)

Instability mechanisms in supersonic base flows. / Sandberg, R. D.; Fasel, Hermann F.

AIAA Paper. 2004. p. 5803-5814.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Sandberg, RD & Fasel, HF 2004, Instability mechanisms in supersonic base flows. in AIAA Paper. pp. 5803-5814, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, 1/5/04.
Sandberg RD, Fasel HF. Instability mechanisms in supersonic base flows. In AIAA Paper. 2004. p. 5803-5814
Sandberg, R. D. ; Fasel, Hermann F. / Instability mechanisms in supersonic base flows. AIAA Paper. 2004. pp. 5803-5814
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