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

J. Cui; R. K. Agarwal

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 proceeding › Conference contribution › peer-review

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 language	English
Title of host publication	35th AIAA Fluid Dynamics Conference and Exhibit
State	Published - 2005
Event	35th AIAA Fluid Dynamics Conference and Exhibit - Toronto, ON, Canada Duration: Jun 6 2005 → Jun 9 2005

Publication series

Name	35th AIAA Fluid Dynamics Conference and Exhibit

Conference

Conference	35th AIAA Fluid Dynamics Conference and Exhibit
Country/Territory	Canada
City	Toronto, ON
Period	06/6/05 → 06/9/05

Cite this

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

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.",

author = "J. Cui and Agarwal, \{R. K.\}",

year = "2005",

language = "English",

isbn = "9781624100598",

series = "35th AIAA Fluid Dynamics Conference and Exhibit",

booktitle = "35th AIAA Fluid Dynamics Conference and Exhibit",

note = "35th AIAA Fluid Dynamics Conference and Exhibit ; Conference date: 06-06-2005 Through 09-06-2005",

}

TY - GEN

T1 - CFD validation of turbulent separation control on a 2D hump (NASA Langley Workshop Validation: Case 3)

AU - Cui, J.

AU - Agarwal, R. K.

PY - 2005

Y1 - 2005

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/84884945252

M3 - Conference contribution

AN - SCOPUS:84884945252

SN - 9781624100598

T3 - 35th AIAA Fluid Dynamics Conference and Exhibit

BT - 35th AIAA Fluid Dynamics Conference and Exhibit

T2 - 35th AIAA Fluid Dynamics Conference and Exhibit

Y2 - 6 June 2005 through 9 June 2005

ER -

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

Abstract

Publication series

Conference

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