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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
- 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