Experimental and numerical study on the interaction of shock wave with helium bubble in shock tube
huang jia1; jia hong-yin1; luo xi-sheng1; yang ji-ming1; zou li-yong2; tan duo-wang2(1.dept.modern mechanics; university of science and technology of china; hefei 230027; china; 2.national key laboratory for shock wave and detonation physics; institute of fluid physics; caep; mianyang sichuan 621900; china)
Flow visualization of butterfly hovering fly via a mechanical model
huang shuo-qiao1; shen gong-xin1; wei lai2; guo peng1(1.institute of fluid dynamics; beijing university of aeronautics and astronautics; beijing 100191; china; 2.china precision engineering institute for aircraft industry; beijing 100076; china)
Study on the characteristics of fore-body separate flow at high angle of attack under plasma control
wang jian-lei1; li hua-xing1; meng xuan-shi1liu feng2; luo shi-jun2(1.national key laboratory of aerodynamics design and research; northwestern polytechnical university; xi an 710072; china; 2.the department of mechanical and aerospace engineering; university of california irvine; irvine ca 92697-3975; usa)
The contrastive study of the process of gasoline liquid-film spray and cylindrical spray with PIV measurements
liu gang1; wang yang2; xu xiang1; wang zhi-qiang3; dong su-rong1; pi jun4(1.automobile engineering department; academy of military transportation; tianjin 300161; china; 2.state key laboratory of engines; tianjin university; tianjin 300072; china; 3.xiangfan branch of academy of military economy; xiangfan; 441118; china; 4.training division; academy of military transportation; tianjin 300161; china)