A Test Research in Wind Tunnel for Aerodynamic Loads Effect on Separation Trajectories of The Internal Missile of Fighter
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引用本文: | 王勋年, 李军, 刘晓晖. 空气动力对飞机内藏式导弹分离轨迹影响的低速风洞试验研究[J]. 实验流体力学, 1999, 13(2): 38-43. DOI: 10.3969/j.issn.1672-9897.1999.02.006 |
Citation: | Wang Xunnian, Li Jun, Liu Xiaohui. A Test Research in Wind Tunnel for Aerodynamic Loads Effect on Separation Trajectories of The Internal Missile of Fighter[J]. Journal of Experiments in Fluid Mechanics, 1999, 13(2): 38-43. DOI: 10.3969/j.issn.1672-9897.1999.02.006 |