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Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - trailing-edge flaps deflected

机译：风速隧道调查在马赫数为0.50至1.29的未扫描锥形翼长宽比2.67，带有前缘和后缘襟翼 - 后缘襟翼偏转

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作者
Stivers, Louis S , Jr; Malick, Alexander W;
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年度 1950
页码 1-50
总页数 50
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Effects of Leading- and Trailing-Edge Gurney Flaps on a Delta Wing [J] . Lance W. Traub, Samuel F. Galls Journal of Aircraft . 1999,第4期

机译：前缘和后缘格尼襟翼对三角翼的影响
2. Wind-Tunnel Testing of Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction [J] . Beatrice Roget, Inderjit Chopra Journal of Aircraft . 2008,第3期

机译：带有独立控制后缘襟翼的转子风洞测试，用于减振
3. Continuous Robust Control for Two-Dimensional Airfoils with Leading- and Trailing-Edge Flaps [J] . Z. Wang, A. Behal, P. Marzocca Journal of guidance, control, and dynamics . 2012,第2期

机译：具有前缘和后缘襟翼的二维机翼的连续鲁棒控制
4. Aerodynamic Optimization of Mach 0.745 Transonic Truss-Braced Wing Aircraft with Variable-Camber Continuous Trailing-Edge Flap [C] . Juntao Xiong, Robert E. Bartels, Nhan Nguyen AIAA SciTech Forum and Exposition . 2021

机译：MACH 0.745跨安桁架支架翼飞机的空气动力学优化，可变弧形连续后缘襟翼
5. Unsteady airfoil flow control via a dynamically deflected trailing-edge flap. [D] . Gerontakos, Panayiote. 2008

机译：通过动态偏转的后缘襟翼进行不稳定的翼型流量控制。
6. Continuous Robust Control for Two-Dimensional Airfoils with Leading- and Trailing-Edge Flaps [O] . Z. Wang, A. Behal, P. Marzocca 2012

机译：具有前缘和后缘襟翼的二维翼型的连续鲁棒控制

Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - trailing-edge flaps deflected

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