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Article Navigation >  Journal of Experiments in Fluid Mechanics  > 2011  >  25(3): 50-55
SUN Hai-sheng, ZHU Ming-hong, HUANG Yong, et al. Key technique for high angle of attack test of fighter aircraft in Φ3.2m low speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(3): 50-55. doi: 10.3969/j.issn.1672-9897.2011.03.012
Citation: SUN Hai-sheng, ZHU Ming-hong, HUANG Yong, et al. Key technique for high angle of attack test of fighter aircraft in Φ3.2m low speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(3): 50-55. doi: 10.3969/j.issn.1672-9897.2011.03.012
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Key technique for high angle of attack test of fighter aircraft in Φ3.2m low speed wind tunnel

doi: 10.3969/j.issn.1672-9897.2011.03.012

  • Publish Date: 2011-06-25

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