Investigation of the Effect of Thickness Taper Ratio and Aspect Ratio on Fin Flutter Velocity of a Model Rocket using Response Surface Method | AVESİS

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Investigation of the Effect of Thickness Taper Ratio and Aspect Ratio on Fin Flutter Velocity of a Model Rocket using Response Surface Method

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CEYHUN T., NİKBAY M.

7th International Conferenceon Recent Advances in Space Technologies, İstanbul, Turkey, 16 - 19 June 2015

Publication Type: Conference Paper / Full Text
City: İstanbul
Country: Turkey
Istanbul Technical University Affiliated: No