INFLUENCE OF AFTERBODY ROUNDING ON THE PRESSURE DRAG OF AN AXISYMMETRICAL BLUFF-BODY

Citation
G. Buresti et al., INFLUENCE OF AFTERBODY ROUNDING ON THE PRESSURE DRAG OF AN AXISYMMETRICAL BLUFF-BODY, Journal of wind engineering and industrial aerodynamics, 71, 1997, pp. 179-188
Citations number
6
ISSN journal
01676105
Volume
71
Year of publication
1997
Pages
179 - 188
Database
ISI
SICI code
0167-6105(1997)71:<179:IOAROT>2.0.ZU;2-6
Abstract
The effects of rounding the aft edges of a blunt-based axisymmetrical bluff body with streamlined forebody are studied by means of surface-p ressure measurements, at Reynolds numbers (based on the model length) Re-L = 1.15 x 10(6) and Re-L = 2.88 x 10(6). The results show that for a certain of curvature a maximum in pressure drag occurs, connected w ith the variation of the pressures on the portion of the afterbody lyi ng inside the separated wake, and with the contribution of the suction peaks before separation. However, the behaviour of the drag is found to be significantly dependent on Reynolds number, while the forcing of the boundary-layer transition at a fixed upstream position produces a substantial decrease of the drag only for the lower tests velocity.