3-D CFD validation of an axisymmetric jet in cross-flow (NASA Langley Workshop Validation: Case 2)

J. Cui, R. K. Agarwal

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

3 Scopus citations

Abstract

An Unsteady Reynolds-Averaged Navier-Stokes (URANS) solver - WIND is employed to compute the flow field of an axisymmetric synthetic jet in cross-flow. This flow field corresponds to case 2 of NASA Langley Research Center Workshop "CFD validation of synthetic jets and turbulent separation control" held at Williamsburg, VA in March 2004. Three-dimensional simulations of case 2 have been performed by employing the appropriate boundary conditions at the diaphragm of the actuator using SST, SA and DES turbulence models. The numerical simulations are compared with the experimental data; fair agreement is obtained.

Original languageEnglish (US)
Title of host publication43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers
Pages425-433
Number of pages9
StatePublished - 2005
Externally publishedYes
Event43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States
Duration: Jan 10 2005Jan 13 2005

Other

Other43rd AIAA Aerospace Sciences Meeting and Exhibit
CountryUnited States
CityReno, NV
Period1/10/051/13/05

ASJC Scopus subject areas

  • Engineering(all)

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    Cui, J., & Agarwal, R. K. (2005). 3-D CFD validation of an axisymmetric jet in cross-flow (NASA Langley Workshop Validation: Case 2). In 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers (pp. 425-433)