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Article Navigation >  Journal of Experiments in Fluid Mechanics  > 1999  >  13(2): 38-43
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
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
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A Test Research in Wind Tunnel for Aerodynamic Loads Effect on Separation Trajectories of The Internal Missile of Fighter

doi: 10.3969/j.issn.1672-9897.1999.02.006

  • Publish Date: 1999-02-01

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