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Transonic flutter investigation of an all-moveable horizontal tail for a fighter airplane

机译：用于战斗机飞机的全动水平尾翼的跨音速颤振研究

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Land, Norman S; Abbott, Rank T , Jr;
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年度 1957
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
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专利

1. NONLINEAR AERODYNAMIC EFFECTS ON TRANSONIC FLAP BUZZ, TAIL FLUTTER AND LIMIT-CYCLE OSCILLATIONS OF TWO-DIMENSIONAL WING-FLAP-TAIL CONFIGURATIONS [J] . J.-C. Cheng The Chinese journal of mechanics . 2009,第4期

机译：二维机翼-襟翼-尾翼构造对跨音速襟翼，尾翼颤动和极限周期振动的非线性气动影响
2. Adaptive Flutter Suppression for a Fighter Wing via Recurrent Neural Networks over a Wide Transonic Range [J] . Liu Haojie, Zhao Yonghui, Hu Haiyan International journal of aerospace engineering . 2016,第pta1期

机译：通过跨跨音速范围的递归神经网络对战斗机机翼进行自适应颤振抑制
3. NUMERICAL INVESTIGATIONS OF THE EFFECT OF AEROELASTIC DEFORMATIONS OF THE WING ON THE AERODYNAMIC CHARCATERISTICS OF THE HALF-MODEL OF AN AIRPLANE AT TRANSONIC SPEED [J] . V. A. Barinov, O. V. Pavlenko, V. V. Yanin TsAGI science journal . 2016,第3期

机译：机翼气动变形对跨音速飞机半模气动特性影响的数值研究
4. NUMERICAL SIMULATION AND WIND TUNNEL TESTING OF FLUTTER ABOUT AN ALL- MOVABLE HORIZONTAL TAIL AT TRANSONIC SPEEDS [C] . Qian Wei, Yang Guowei, Zheng Guannan, Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：跨声速全动水平尾翼颤振的数值模拟与风洞试验
5. Expanding a flutter envelope using data from accelerating flight: Application to the F-16 fighter aircraft. [D] . Harris, Charles A. 2004

机译：使用来自加速飞行的数据来扩大颤振包络：在F-16战斗机上的应用。
6. DNA sequences of the tail fiber genes of bacteriophage P2: evidence for horizontal transfer of tail fiber genes among unrelated bacteriophages. [O] . E Haggård-Ljungquist, C Halling, R Calendar 1992

机译：P2噬菌体尾纤维基因的DNA序列：在无关的噬菌体之间水平转移尾纤维基因的证据。
7. Contributions of Transonic Dynamics Tunnel Testing to Airplane Flutter Clearance [O] . Florance James R., Rivera Jose A. 2000

机译：跨音速动力学隧道测试对飞机颤振间隙的贡献

Transonic flutter investigation of an all-moveable horizontal tail for a fighter airplane

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