The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet

doi:10.3969/j.issn.1672-9897.2004.02.022

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The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(2): 98-101. doi: 10.3969/j.issn.1672-9897.2004.02.022

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The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet

doi: 10.3969/j.issn.1672-9897.2004.02.022

Publish Date: 2004-02-01

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通讯作者: 陈斌, bchen63@163.com

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沈阳化工大学材料科学与工程学院沈阳 110142

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The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet

doi: 10.3969/j.issn.1672-9897.2004.02.022

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The engineering prediction method for aerodynamic characteristics of the symmetrical tactical missile configuration with inlet

doi: 10.3969/j.issn.1672-9897.2004.02.022

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