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Heat loss from yawed hot wires at subsonic Mach numbers
| Content Provider | University of North Texas |
|---|---|
| Author | Sandborn, Virgil A. Laurence, James C. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | "Heat-loss data at angles of yaw and fixed subsonic Mach numbers for several wires of different diameters commonly used in hot-wire anemometry are presented. Possible methods of correlating the data are examined. The relation of the Reynolds number normal to the flow, which has been used by most researchers, was inadequate except near a Mach number of zero" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc57772 |
| Language | English |
| Publisher Date | 2018-06-29 |
| Access Restriction | Open |
| Subject Keyword | hot-wire anemometry heat loss |
| Content Type | Text |
| Resource Type | Report |
