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 - http://www.scopus.com/inward/record.url?scp=84884945252&partnerID=8YFLogxK
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 -