Jan Navrátil, Adam Jirásek, Peter Hamlington, Lt. Col. Andrew Lofthouse

DOI Number: N/A

Conference number: IFASD-2017-142

This paper presents results of the second Aeroelastic Prediction Workshop which uses the Benchmark Super-Critical Wing, BSCW at flutter conditions as a common test case. The primary purpose of this study is to evaluate the effect of angle of attack. To do so, we analyzed BSCW wing at three angles of attack α = 0deg, α = 1deg and α = 5deg. The second task is to evaluate the effect of gas composition on flutter boundary. The two gases are R-12 heavy gas, used as a test medium for the wind tunnel test, and air.

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In Categories: 1. IFASD 2017, 1.Events, Computational Aeroelasticity
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