Method study on wing-body interference coefficient for missiles with arbitrary shape cross section

doi:10.3969/j.issn.1672-9897.2003.04.019

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Article Navigation > Journal of Experiments in Fluid Mechanics > 2003 > 17(4): 96-98

Method study on wing-body interference coefficient for missiles with arbitrary shape cross section[J]. Journal of Experiments in Fluid Mechanics, 2003, 17(4): 96-98. doi: 10.3969/j.issn.1672-9897.2003.04.019

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Method study on wing-body interference coefficient for missiles with arbitrary shape cross section

doi: 10.3969/j.issn.1672-9897.2003.04.019

Publish Date: 2003-04-01

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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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Method study on wing-body interference coefficient for missiles with arbitrary shape cross section

doi: 10.3969/j.issn.1672-9897.2003.04.019

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Method study on wing-body interference coefficient for missiles with arbitrary shape cross section

doi: 10.3969/j.issn.1672-9897.2003.04.019

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