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Boundary-layer influences on the subsonic near-wake of bluff bodies

Boundary-layer influences on the subsonic near-wake of bluff bodies

Authors :
Britcher, Colin P.
Alcorn, Chrles W.
Source :
Journal of Aircraft. March-April, 1994, Vol. 31 Issue 2, p443, 2 p.
Publication Year :
1994

Abstract

The subsonic near-wake of a class of slanted-base bluff bodies has been examined. The incoming boundary-layer momentum thickness affects base pressure and wake stagnation point locations. If the Reynolds number based on the Re(theta) value is selected as the independent factor, than resemblance is evident.

Details

ISSN :
00218669
Volume :
31
Issue :
2
Database :
Gale General OneFile
Journal :
Journal of Aircraft
Publication Type :
Academic Journal
Accession number :
edsgcl.15460399