Simulations of high speed impinging jets

Chris C. Nelson, Alan B. Cain, Philip J. Morris

Research output: Contribution to conferencePaperpeer-review

5 Scopus citations

Abstract

Time accurate simulation of a high speed impinging jet configuration was performed using both the RANS-based Wind-US production flow solver and the CHOPA computational aeroacoustics solver. Qualitatively, the Wind-US solution predicted many of the major features observed experimentally for this flow. Though direct comparison with experiment was not possible, the predicted peak sound pressure level and frequency appears reasonable in light of the published observations. The observed helical character of the jet plume was also predicted, at least in part. Our initial efforts to model this flow with the CHOPA solver, while not complete, are beginning to produce reasonable-looking results, though a full assessment is not possible until the simulation is complete.

Original languageEnglish (US)
DOIs
StatePublished - Dec 1 2012
Event50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Nashville, TN, United States
Duration: Jan 9 2012Jan 12 2012

Other

Other50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Country/TerritoryUnited States
CityNashville, TN
Period1/9/121/12/12

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Simulations of high speed impinging jets'. Together they form a unique fingerprint.

Cite this