Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(4): 62-66. DOI: 10.3969/j.issn.1672-9897.2004.04.014
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Citation:
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Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(4): 62-66. DOI: 10.3969/j.issn.1672-9897.2004.04.014
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Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(4): 62-66. DOI: 10.3969/j.issn.1672-9897.2004.04.014
|
Citation:
|
Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(4): 62-66. DOI: 10.3969/j.issn.1672-9897.2004.04.014
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