DENG Fan, CHEN Shao-song, TAN Xian-zhong, XU Tao. Investigation of aerodynamic characteristics of canard-configuration missile with different tails in transonic and supersonic flow[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(2): 46-50. DOI: 10.3969/j.issn.1672-9897.2010.02.010
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Citation:
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DENG Fan, CHEN Shao-song, TAN Xian-zhong, XU Tao. Investigation of aerodynamic characteristics of canard-configuration missile with different tails in transonic and supersonic flow[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(2): 46-50. DOI: 10.3969/j.issn.1672-9897.2010.02.010
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DENG Fan, CHEN Shao-song, TAN Xian-zhong, XU Tao. Investigation of aerodynamic characteristics of canard-configuration missile with different tails in transonic and supersonic flow[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(2): 46-50. DOI: 10.3969/j.issn.1672-9897.2010.02.010
|
Citation:
|
DENG Fan, CHEN Shao-song, TAN Xian-zhong, XU Tao. Investigation of aerodynamic characteristics of canard-configuration missile with different tails in transonic and supersonic flow[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(2): 46-50. DOI: 10.3969/j.issn.1672-9897.2010.02.010
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