日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
Bluff bodyの抵抗減少と後流
末松 良勝相原 康彦
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ジャーナル フリー

1982 年 30 巻 341 号 p. 321-328

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抄録
This paper describes an experimental study on the near wake behind bluff body in relation to the base drag reduction. The experiments were carried out using the models with two-dimensional blunt trailing edge and with periodically three-dimensional one. REYNOLDS number based on uniform velocity and base thickness is lessthan 8×103.
Behind the two-dimensional bluff body, the periodic vortex shedding occurs and the static pressure reduces in the vortex formation region. In the case of the three-dimensional model, it is observed as a general tendency that the static pressure reduction and the concentration of periodic vortices are not notable. This seems to be the essential feature associated with the drag reduction of three-dimensional bluff body.
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© The Japan Society for Aeronautical and Space Sciences
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