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Empty test section streamlining of the transonic self-streamlining wind tunnel fitted with new walls
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lewis, M. C. |
| Copyright Year | 1988 |
| Description | The original flexible top and bottom walls of the Transonic Self-Streamlining Wind Tunnel (TSWT), at the University of Southampton, have been replaced with new walls featuring a larger number of static pressure tappings and detailed mechanical improvements. This report describes the streamling method, results, and conclusions of a series of tests aimed at defining sets of aerodynamically straight wall contours for the new flexible walls. This procedure is a necessary prelude to model testing. The quality of data obtained compares favorably with the aerodynamically straight data obtained with the old walls. No operational difficulties were experienced with the new walls. |
| File Size | 688453 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880016058 |
| Archival Resource Key | ark:/13960/t05x76x8r |
| Language | English |
| Publisher Date | 1988-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Wind Tunnels Wind Tunnel Tests Wind Tunnel Walls Streamlining Two Dimensional Flow Aerodynamic Forces Flexibility Adaptive Control Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |