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Flutter tests (os1) of the 0.02-scale shuttle orbiter wing/elevon semi-span model 230
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kotch, M. H. |
| Copyright Year | 1974 |
| Description | A series of simple wing/elevon flutter models of the shuttle orbiter were tested in a 26-inch transonic blowdown tunnel. Flutter points were obtained for two levels of scaled elevon actuator stiffness. A description of the wind tunnel models and the test procedures utilized in the experiment are given. |
| File Size | 2503550 |
| Page Count | 70 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740012436 |
| Archival Resource Key | ark:/13960/t6b32n46w |
| Language | English |
| Publisher Date | 1974-02-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Subsonic Speed Elevons Blowdown Wind Tunnels Wind Tunnel Tests Transonic Speed Wind Tunnel Models Aeroelasticity Space Shuttle Orbiters Graphs Charts Transonic Flutter Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
