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

Research output: Contribution to conferencePaperpeer-review

9 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
Pages425-433
Number of pages9
StatePublished - 2005
Event43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States
Duration: Jan 10 2005Jan 13 2005

Conference

Conference43rd AIAA Aerospace Sciences Meeting and Exhibit
Country/TerritoryUnited States
CityReno, NV
Period01/10/0501/13/05

Fingerprint

Dive into the research topics of '3-D CFD validation of an axisymmetric jet in cross-flow (NASA Langley Workshop Validation: Case 2)'. Together they form a unique fingerprint.

Cite this