CFD validation of turbulent separation control on a 2D hump (NASA Langley Workshop Validation: Case 3)

J. Cui, R. K. Agarwal

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

1 Scopus citations

Abstract

An Unsteady Reynolds-Averaged Navier-Stokes (URANS) solver - WIND is employed to compute the flow field resulting from active control of turbulent separation over a nominal 2D hump using a synthetic jet actuator. This flow field corresponds to case 3 of NASA Langley Research Center Workshop "CFD validation of synthetic jets and turbulent separation control" held at Williamsburg, VA in March 2004.1 In this paper, the results of detailed calculations for this case are presented along with their comparison with experimental data.

Original languageEnglish (US)
Title of host publication35th AIAA Fluid Dynamics Conference and Exhibit
StatePublished - 2005
Externally publishedYes
Event35th AIAA Fluid Dynamics Conference and Exhibit - Toronto, ON, Canada
Duration: Jun 6 2005Jun 9 2005

Other

Other35th AIAA Fluid Dynamics Conference and Exhibit
CountryCanada
CityToronto, ON
Period6/6/056/9/05

ASJC Scopus subject areas

  • Engineering (miscellaneous)
  • Aerospace Engineering

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    Cui, J., & Agarwal, R. K. (2005). CFD validation of turbulent separation control on a 2D hump (NASA Langley Workshop Validation: Case 3). In 35th AIAA Fluid Dynamics Conference and Exhibit