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
|
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
|
DownLoad: