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Unit-Reynolds-number effects on boundary-layer transition
- Source :
- AIAA Journal. Jan, 1993, Vol. 31 Issue 1, p195, 2 p.
- Publication Year :
- 1993
-
Abstract
- The effects of increasing Reynolds number on the boundary-layer transition of turbulent flows is investigated. Planar and conical boundary-layer transition are compared at aMach number of eight to obtain the unit-Reynolds number effects. Hot-wire anemometry experiments are also conducted at the same Mach number. Results showthat the cone transitin data obtained produces a unit-Reynolds-number that is steeper than the wind-tunnel planar slope.
Details
- ISSN :
- 00011452
- Volume :
- 31
- Issue :
- 1
- Database :
- Gale General OneFile
- Journal :
- AIAA Journal
- Publication Type :
- Academic Journal
- Accession number :
- edsgcl.13865152