SUN Hai-sheng, ZHU Ming-hong, HUANG Yong, LIU Zhi-tao. 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, LIU Zhi-tao. 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
|
SUN Hai-sheng, ZHU Ming-hong, HUANG Yong, LIU Zhi-tao. 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, LIU Zhi-tao. 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
|
DownLoad: