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

J. Cui; R. K. Agarwal

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

J. Cui
, R. K. Agarwal

Research output: Contribution to conference › Paper › peer-review

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 language	English
Pages	425-433
Number of pages	9
State	Published - 2005
Event	43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: Jan 10 2005 → Jan 13 2005

Conference

Conference	43rd AIAA Aerospace Sciences Meeting and Exhibit
Country/Territory	United States
City	Reno, NV
Period	01/10/05 → 01/13/05

Cite this

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

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.",

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

year = "2005",

language = "English",

pages = "425--433",

note = "43rd AIAA Aerospace Sciences Meeting and Exhibit ; Conference date: 10-01-2005 Through 13-01-2005",

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T1 - 3-D CFD validation of an axisymmetric jet in cross-flow (NASA Langley Workshop Validation: Case 2)

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 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/30744471191

M3 - Paper

AN - SCOPUS:30744471191

SP - 425

EP - 433

T2 - 43rd AIAA Aerospace Sciences Meeting and Exhibit

Y2 - 10 January 2005 through 13 January 2005

ER -

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

Abstract

Conference

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