Abstract
The Reynolds-averaged Navier-Stokes (RANS) equations and detached-eddy simulation (DES) were used for calculating the flowfield around 6:1 prolate spheroid at angle of attack. The calculations were performed at a Reynolds number of 4.2×10 6, the flow was tripped at x/L=0.2, and the angle of attack α was varied from 10 to 20 deg. The Spalart-Allmaras one-equation model was used for the RANS calculations. Corrections for streamline curvature improve prediction of the pressure coefficient in the separated region on the leeward side of the spheroid.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 904-910 |
| Number of pages | 7 |
| Journal | Journal of Fluids Engineering, Transactions of the ASME |
| Volume | 124 |
| Issue number | 4 |
| DOIs | |
| State | Published - Dec 2002 |
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ASJC Scopus subject areas
- Mechanical Engineering
- Fluid Flow and Transfer Processes
Cite this
Numerical investigation of flow past a prolate spheroid. / Constantinescu, George S.; Pasinato, Hugo; Wang, You Qin; Forsythe, James R.; Squires, Kyle.
In: Journal of Fluids Engineering, Transactions of the ASME, Vol. 124, No. 4, 12.2002, p. 904-910.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Numerical investigation of flow past a prolate spheroid
AU - Constantinescu, George S.
AU - Pasinato, Hugo
AU - Wang, You Qin
AU - Forsythe, James R.
AU - Squires, Kyle
PY - 2002/12
Y1 - 2002/12
N2 - The Reynolds-averaged Navier-Stokes (RANS) equations and detached-eddy simulation (DES) were used for calculating the flowfield around 6:1 prolate spheroid at angle of attack. The calculations were performed at a Reynolds number of 4.2×10 6, the flow was tripped at x/L=0.2, and the angle of attack α was varied from 10 to 20 deg. The Spalart-Allmaras one-equation model was used for the RANS calculations. Corrections for streamline curvature improve prediction of the pressure coefficient in the separated region on the leeward side of the spheroid.
AB - The Reynolds-averaged Navier-Stokes (RANS) equations and detached-eddy simulation (DES) were used for calculating the flowfield around 6:1 prolate spheroid at angle of attack. The calculations were performed at a Reynolds number of 4.2×10 6, the flow was tripped at x/L=0.2, and the angle of attack α was varied from 10 to 20 deg. The Spalart-Allmaras one-equation model was used for the RANS calculations. Corrections for streamline curvature improve prediction of the pressure coefficient in the separated region on the leeward side of the spheroid.
UR - http://www.scopus.com/inward/record.url?scp=10844277461&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=10844277461&partnerID=8YFLogxK
U2 - 10.1115/1.1517571
DO - 10.1115/1.1517571
M3 - Article
AN - SCOPUS:10844277461
VL - 124
SP - 904
EP - 910
JO - Journal of Fluids Engineering, Transactions of the ASME
JF - Journal of Fluids Engineering, Transactions of the ASME
SN - 0098-2202
IS - 4
ER -