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Automation And Verification Of Ankara Wind Tunnel

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.

Identiferoai:union.ndltd.org:METU/oai:etd.lib.metu.edu.tr:http://etd.lib.metu.edu.tr/upload/12607692/index.pdf
Date01 September 2003
CreatorsKatirci, Argun
ContributorsAlemdaroglu, Nafiz
PublisherMETU
Source SetsMiddle East Technical Univ.
LanguageEnglish
Detected LanguageEnglish
TypeM.S. Thesis
Formattext/pdf
RightsTo liberate the content for public access

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