All the operational and measurement systems of Ankara Wind Tunnel was modified to
operate automatically under the control of a central computer system programmed using
the Lab View programming language.
A cruciform air-to-air missile with triangular canard control and a trapezoidal wing
model was tested by a 35mm diameter internal balance at Mach 0.2 and data was
compared with the test data of the same model&rsquo / s test that was performed at NASA
Langley Research Center.
| Identifer | oai:union.ndltd.org:METU/oai:etd.lib.metu.edu.tr:http://etd.lib.metu.edu.tr/upload/12607692/index.pdf |
| Date | 01 September 2003 |
| Creators | Katirci, Argun |
| Contributors | Alemdaroglu, Nafiz |
| Publisher | METU |
| Source Sets | Middle East Technical Univ. |
| Language | English |
| Detected Language | English |
| Type | M.S. Thesis |
| Format | text/pdf |
| Rights | To liberate the content for public access |
Page generated in 0.0018 seconds