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Calibration of the langley 16-foot transonic tunnel with test section air removal
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Corson Jr., B. W. Igoe, W. B. Runckel, J. F. |
| Copyright Year | 1974 |
| Description | The Langley 16-foot transonic tunnel with test section air removal (plenum suction) was calibrated to a Mach number of 1.3. The results of the calibration, including the effects of slot shape modifications, test section wall divergence, and water vapor condensation, are presented. A complete description of the wind tunnel and its auxiliary equipment is included. |
| File Size | 5936809 |
| Page Count | 117 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740026564 |
| Archival Resource Key | ark:/13960/t7vm91c2d |
| Language | English |
| Publisher Date | 1974-08-01 |
| Access Restriction | Open |
| Subject Keyword | Slots Transonic Wind Tunnels Flow Characteristics Wind Tunnel Apparatus Water Vapor Wind Tunnel Calibration Mach Number Exhaust Systems 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 |