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Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile

机译：双模振荡幅度频率特性对对称翼型跨越横向流线的单侧表面效应

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V. P. Zamuraev; A. P. Kalinina;
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1. Nonlinear effects in the interaction of periodic pulsed energy supply and shock-wave structure during transonic streamlining of wing profiles [J] . Aulchenko SM, Zamuraev VP, Kalinina AP Technical physics letters: Letters to the Russian journal of applied physics . 2006,第1期

机译：机翼跨音速流线化过程中周期性脉冲能量供应与冲击波结构相互作用的非线性影响
2. NUMERICAL AND ANALYTICAL STUDY OF NONLINEAR EFFECTS OF TRANSONIC FLOW PAST A WING AIRFOIL IN OSCILLATION OF ITS SURFACE ELEMENT [J] . S. M. Aulchenko, V. P. Zamuraev, A. P. Kalinina Journal of engineering physics and thermophysics . 2014,第3期

机译：跨翼流翼型翼型在其表面元素振荡中的非线性效应的数值和分析研究
3. Computational aeroelastic investigation of a transonic limit-cycle-oscillation experiment at a transport aircraft wing model [J] . Bernd Stickan, Johannes Dillinger, Gunter Schewe Journal of Fluids and Structures . 2014,第Null期

机译：运输机翼模型中跨音速极限循环振荡实验的计算气动弹性研究
4. Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile [C] . V. P. Zamuraev, A. P. Kalinina International Conference on the Methods of Aerophysical Research . 2018

机译：双模振荡幅度频率特性对对称翼型跨越横向流线的单侧表面效应
5. Aerodynamic performance of transonic and subsonic airfoils: Effects of surface roughness, turbulence intensity, Mach number, and streamline curvature-airfoil shape. [D] . Zhang, Qiang. 2005

机译：跨音速和亚音速机翼的空气动力学性能：表面粗糙度，湍流强度，马赫数和流线曲率翼型的影响。
6. Correction: Hydrophobic durability characteristics of butterfly wing surface after freezing cycles towards the design of nature inspired anti-icing surfaces [O] . -1

机译：更正：蝴蝶机翼表面经过自然设计的防冰表面冻结循环后的疏水性耐久性能
7. Measured unsteady transonic aerodynamic characteristics of an elastic supercritical wing with an oscillating control surface [O] . D. SEIDEL, M. SANDFORD, C. ECKSTROM 1985

机译：用振荡控制表面测量弹性超临界机翼的非稳定跨跨度空气动力学特性
8. A CORRELATION BY MEANS OF THE TRANSONIC SIMILARITY RULES OF THE EXPERIMENTALLY DETERMINED CHARACTERISTICS OF 22 RECTANGULAR WINGS OF SYMMETRICAL PROFILE [R] . John B. McDevitt 1952

机译：关于对称剖面22个矩形翼的实验确定特征的跨音相似规律的相关性

Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile

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