Automation and verification of Ankara wind tunnel

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Date

2006

Author

Katırcı, Argün

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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’s test that was performed at NASA Langley Research Center.

Subject Keywords

Aeronautics.

URI

http://etd.lib.metu.edu.tr/upload/12607692/index.pdf
https://hdl.handle.net/11511/16104

Collections

Graduate School of Natural and Applied Sciences, Thesis

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Citation Formats

A. Katırcı, “Automation and verification of Ankara wind tunnel,” M.S. - Master of Science, Middle East Technical University, 2006.