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Seeing through flows in langley's 0.3-meter transonic cryogenic tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Burner, A. W. Goad, W. K. Snow, W. L. |
| Copyright Year | 1982 |
| Description | Viewing problems associated with the measurement of model deformation in cryogenic wind tunnels are discussed. Tests were conducted in the Langley 0.3-Meter Transonic Cryogenic Tunnel to assess viewing capabilities thru the flow field. The effects of condensation and turbulent boundary layers are discussed and a modelling procedure for image degradation is described. |
| File Size | 569000 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820024802 |
| Archival Resource Key | ark:/13960/t6rz43b1n |
| Language | English |
| Publisher Date | 1982-09-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Effects Deformation Viewing Transonic Wind Tunnels Condensing Turbulent Boundary Layer Visibility Wind Tunnel Models Cryogenic Wind Tunnels High Pressure Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |