【摘要】：有翼高超聲速飛行器已取得了較為廣泛的應(yīng)用,有翼高超聲速飛行器復(fù)雜翼舵干擾對(duì)飛行器氣動(dòng)特性有很大的影響。半個(gè)世紀(jì)以來(lái),高超聲速翼舵干擾集中在鴨翼與主翼的氣動(dòng)干擾研究,而針對(duì)主翼與全動(dòng)舵氣動(dòng)干擾的研究較少。對(duì)主翼與舵干擾、鴨翼與主翼干擾氣動(dòng)特性研究現(xiàn)狀進(jìn)行了概述,并對(duì)翼舵干擾的關(guān)鍵問(wèn)題進(jìn)行了總結(jié)。
[Abstract]:The winged hypersonic vehicle has been widely used. The complex wing rudder interference of the winged hypersonic vehicle has a great influence on the aerodynamic characteristics of the aircraft. For half a century, hypersonic wing rudder interference has focused on the pneumatic interference between duck wing and main wing, while the research on main wing and fully moving rudder has been less. The research status of main wing and rudder interference, duck wing and main wing interference is summarized, and the key problems of wing and rudder interference are summarized.
【作者單位】： 北京航空航天大學(xué);
【分類(lèi)號(hào)】：TJ760;V211
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本文編號(hào)：2507447