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Cryogenic wind tunnel activities at the university of southampton. [flow visusalization technique for low speed wind tunnel tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Goodyer, M. J. |
| Copyright Year | 1979 |
| Description | The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide band of usable Reynolds numbers is analyzed along with a flow visualization technique using propane. The combination of magnetic suspension with the cryogenic wind tunnel is described. An outline of the circuit showing the locations of the magnet system and the features of the tunnel are presented. |
| File Size | 291734 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800001991 |
| Archival Resource Key | ark:/13960/t20c9rp6h |
| Language | English |
| Publisher Date | 1979-09-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Temperature Effects Thermocouples Reynolds Number Wind Tunnel Tests Flow Visualization Low Speed Wind Tunnels Cryogenic Wind Tunnels Magnetic Suspension Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |