[FKFU-A280-00-A] FloEFD Aerospace Validation Cases : M-165 CANARD/WING/BODY RESEARCH MODEL AT 0.7<M<1.35
작성자
플로우마스터코리아
작성일
2021-10-28 15:03
조회
47
A simple canard/wing/body research model with a low aspect ratio (2.3), highly swept (58º) wing with leading-edge 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.