Aerodynamic hysteresis in the model of an airplane with a high-aspect-ratio straight wing

Kolin IV; Svyatodukh VK; Trifonova TI; Shukhovtsov DV

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Aerodynamic hysteresis in the model of an airplane with a high-aspect-ratio straight wing

机译：高纵横比直翼飞机模型中的气动滞后

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摘要

Many-loop hysteresis of the pitching characteristics of an airplane model with a high-aspect-ratio straight wing at Re = 0.33 x 10(6) is studied.

机译：研究了高纵横比直翼飞机模型在Re = 0.33 x 10（6）时的俯仰特性的多环滞后现象。

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来源
《Technical physics》 |2006年第4期|共4页
作者
Kolin IV; Svyatodukh VK; Trifonova TI; Shukhovtsov DV;
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原文格式 PDF
正文语种 eng
中图分类物理学;
关键词
51; 10; +y;

机译：51;10;+和;

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专利

1. Aerodynamic hysteresis in the model of an airplane with a high-aspect-ratio straight wing [J] . Kolin IV, Svyatodukh VK, Trifonova TI, Technical physics . 2006,第4期

机译：高纵横比直翼飞机模型中的气动滞后
2. Rotary Aerodynamic Derivatives in the Asymptotic Theory of a High-Aspect-Ratio Wing [J] . A. N. Khrabrov Fluid Dynamics . 2007,第1期

机译：高纵横比机翼渐近理论中的旋转气动导数
3. On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings [J] . M. J. Patil, D. H. Hodges Journal of Fluids and Structures . 2004,第7期

机译：空气动力学和结构几何非线性在高纵横比机翼气动弹性行为中的重要性
4. MODEL MODIFICATION OF TRANSONIC AERODYNAMIC FORCE ON A HIGH-ASPECT-RATIO AEROELASTIC WING AND ITS ACTIVE FLUTTER [C] . A. Fujimori, H. Matsushita, K. Saitoh 22nd international congress of aeronautical sciences (ICAS 2000) . 2000

机译：高纵横比气动弹性翼及其主动颤振上的跨气动力模型修正
5. An investigation of the dynamic effects of flap deflection on the aerodynamic characteristics of an airplane wing using computational fluid dynamics [D] . Moerchel, Alexander M. 2006

机译：利用计算流体力学研究襟翼偏转对飞机机翼空气动力学特性的动态影响
6. A Modified Quasisteady Aerodynamic Model for a Sub-100 mg Insect-Inspired Flapping-Wing Robot [O] . Chenyang Wang, Weiping Zhang, Junqi Hu, 2020

机译：一个改进的Quasisteade气动模型用于SUB-100 MG昆虫启发拍翼机器人
7. Calculation of Aerodynamic Performance Characteristics of Airplane Wing and Comparing with the Experimental Measurement [O] . Haci Sogukpinar, Ismail Bozkurt 2015

机译：飞机翼空气动力学性能特征计算及实验测量比较
8. INVESTIGATION AT LOW SPEEDS OF DEFLECTORS AND SPOILERS AS GUST ALLEVIATORS ON A MODEL OF THE-BELL X-5 AIRPLANE WITH 35° SWEPT WINGS AND ON A HIGH-ASPECT-RATIO 35° SWEPT-WING-FUSELAGE MODEL [R] . Delwin R. Croom, Jarrett K. Huffman 1957

机译：在具有35°sW形翼的X-5型飞机模型上以及在高纵横比35°sWEpT-WING-FUsELaGE模型上作为降噪装置的低速飞行器和瞄准器的调查

Aerodynamic hysteresis in the model of an airplane with a high-aspect-ratio straight wing

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