WordNet
- (especially of aircraft wings) angled rearward from the point of attachment; "aircraft with sweptback wings"
PrepTutorEJDIC
- (飛行機の翼が)後退角を持つ,(飛行機が)後退翼を有する / (髪を)オールバックにした
Japanese Journal
- G050081 低Re数領域で用いる水中グライダーの翼形状に関する研究([G05008]流体工学部門一般セッション(8):流体機器2)
- 江端 重葉,安田 孝宏,南川 久人,里深 信行
- 年次大会 : Mechanical Engineering Congress, Japan 2011, "G050081-1"-"G050081-5", 2011-09-11
- … Planforms of wing of model are rectangle, taper, and sweptback wings, and aerofoils of wing are flat plate, NACA0012, NACA0008, NACA6406, NACA3310, SE4410 which is the cross section shape of flamingo's wing, and Remodeled SE4410 which remodels lower surface of SE4410. …
- NAID 110009758857
- An Experimental Study on the Improvement of Aerodynamic Characteristics of Lifting Body Configuration by Active Flow Control Method
- Tsuchiya Shigeki,Aso Shigeru,Tani Yasuhiro
- Memoirs of the Faculty of Engineering, Kyushu University 68(4), 175-192, 2008-12
- … In the series of experiments the increase of lift coefficient at higher angle of attack and the decrease of drag coefficient at lower angle of attack were observed in some conditions of the location of blowing and the sweptback angle and direction of the nozzle for active flow control. …
- NAID 120001024387
- 後退角の大きくないデルタ翼のロール自励振動
- 中村 佳朗,松野 隆
- 日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences 48(560), 490-494, 2000-09-05
- NAID 10004623381
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