The effect of shoulder radiusing and grooving (longitudinally and circumferentially) the afterbodies of bluff bodies to reduce the base drag at low speeds is investigated experimentally. Shoulder radii as large as 2.75 body diameters are examined. Reynolds number (ReD) based on body diameter varied from 20,000 to 200,000. Results indicate that increasing the shoulder radius to 2.00 body diameters can reduce the drag levels to those of a streamline body having 67 percent greater fineness ratio. For the relatively sharp shoulder case, body drag reductions as large as 50 and 33 percent are obtained using circumferential or longitudinal grooves, respectively.
Axisymmetric bluff-body drag reduction through geometrical modification
Journal of Aircraft ; 22
1985-06-01
Sonstige
Keine Angabe
Englisch
Drag and Wake Modification of Axisymmetric Bluff Bodies Using Coanda Blowing
Online Contents | 1994
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