Morphing Flap Concept to Reduce the Flap Side Edge Noise for Aircraft Wing Slotted Flaps
Morphing Flap Concept to Reduce the Flap Side Edge Noise for Aircraft Wing Slotted Flaps
复制标题
变形襟翼概念可降低飞机机翼开缝襟翼的襟翼侧边缘噪声
DOI:
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复制
发表时间:
2013
期刊:
影响因子:
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通讯作者:
Hiroki Ura and Takeshi Ito
中科院分区:
文献类型:
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作者:
Yasuhiro Tani;Yuya Yamashita;Kazuma Miyazaki;Shigeru Aso;Hiroki Ura and Takeshi Ito