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Streamlining the walls of an empty two-dimensional flexible-walled test section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wolf, S. W. D. Cook, I. D. Goodyer, M. J. |
| Copyright Year | 1982 |
| Description | The techniques used to find aerodynamically straight wall contours in a test section of a transonic wind tunnel are discussed. The walls were defined as aerodynamically straight up to Mach 0.9. |
| File Size | 348301 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820020428 |
| Archival Resource Key | ark:/13960/t20c9s922 |
| Language | English |
| Publisher Date | 1982-05-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Static Pressure Transonic Wind Tunnels Aerodynamics Wind Tunnel Walls Flexibility Displacement Stagnation Pressure Jacks Lifts Tolerances Mechanics Contours Flow Distribution Streamlining Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |