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FloEFD Aerospace Validation Cases : M-165 CANARD/WING/BODY RESEARCH MODEL AT 0.7<M<1.35

posted Oct 19, 2017, 5:52 PM by Songyi Han
A simple canard/wing/body research model with a low aspect ratio (2.3), highly swept (58º) wing with leadingedge
flaps has been tested in the ARA Transonic Wind Tunnel over the range of 0.7<M<1.35 at an incidence of nominally 8º.



▶ 분류 : Whitepaper
▶ 키워드 : 


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