机译:在76/40°双三角翼上大分离流的分离涡模拟
State Key Laboratory of Aerodynamics, Mianyang, Sichuan, 621000, China,National Laboratory of CFD, Beijing University of Aeronautics and Astronautics, Xuanyuan Rd. 37, Haidian District, Beijing, 100191, China;
State Key Laboratory of Aerodynamics, Mianyang, Sichuan, 621000, China,National Laboratory of CFD, Beijing University of Aeronautics and Astronautics, Xuanyuan Rd. 37, Haidian District, Beijing, 100191, China;
State Key Laboratory of Aerodynamics, Mianyang, Sichuan, 621000, China,National Laboratory of CFD, Beijing University of Aeronautics and Astronautics, Xuanyuan Rd. 37, Haidian District, Beijing, 100191, China;
Detached-eddy simulation; Massively separated flows; Double-delta wing; Vortex breakdown; Vortex substructure;
机译:76/40°双倍角翼的新涡流仿真和分析
机译:雷诺数对76/40度双三角翼上流动的影响
机译:有限跨翼周围流动的区域分离涡流模拟
机译:雷诺数对76/40度双三角翼上气流的影响
机译:大规模分离湍流中的涡流检测和跟踪
机译:利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
机译:对76/40度双三角翼上涡流的研究
机译:全飞机经历大规模分离流动的分离涡模拟