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An investigation of the control-surface flutter derivatives of an NACA 65(sub 1)-213 airfoil in the Ames 16-foot high-speed wind tunnel

机译：ames 16英尺高速风洞中NaCa 65（sub 1）-213翼型控制面颤振导数的研究

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Wyss, John A; Sorenson, Robert M;
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年度 1951
页码 1-57
总页数 57
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing's parameters on flutter speed [J] . Thi Tuyet Nhung Le, Chi-Cong Nguyen, Hoang Nam Vang International Journal of Mechanical Engineering and Applications . 2015,第1a3期

机译：低速风洞中NACA0012机翼模型的空气弹性台架试验设计：机翼参数对扑扑速度的影响
2. Modelling of aerodynamic flutter on a NACA 4412 airfoil with application to wind turbine blades [J] . Drishtysingh Ramdenee, Adrian Ilinca, Sorin Ion Minea, International Journal of Simulation & Process Modelling . 2013,第1期

机译：NACA 4412机翼上的气动颤振建模及其在风力涡轮机叶片上的应用
3. Estimation of the flutter derivatives of an NACA airfoil by means of Navier-Stokes simulation [J] . O. P. Le Maitre, R. H. Scanlan, O. M. Knio Journal of Fluids and Structures . 2003,第1期

机译：通过Navier-Stokes模拟估算NACA机翼的颤振导数
4. Investigation of NACA 0012 Airfoil Periodic Flows in a Transonic Wind Tunnel [C] . Xudong Ren, Zijie Zhao, Chao Gao, AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2013

机译：跨音速风洞中NACA 0012翼型周期性流动的研究
5. Direct Numerical Simulations of a Cambered NACA 65(1)-412 Airfoil at Low Reynolds Numbers: Flow Separation, Instabilities and Lagrangian Aerodynamics [D] . Klose, Bjoern Fabian. 2021

机译：低雷诺数的弧形Naca 65（1）-412翼型的直接数值模拟：流动分离，稳定性和拉格朗日空气动力学
6. Airfoil Selection Procedure Wind Tunnel Experimentation and Implementation of 6DOF Modeling on a Flying Wing Micro Aerial Vehicle [O] . Taimur Ali Shams, Syed Irtiza Ali Shah, Ali Javed, 2020

机译：翼型微型飞行器的机翼选择程序风洞实验和6DOF建模实现
7. Numerical and Experimental Investigations on the Meshing Model Choice of a NACA2415 Airfoil Wind Turbine Placed in an Open Wind Tunnel [O] . Zied Driss Tarek Chelbi, Walid Barhoumi Ahmed Kaffel 2015

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An investigation of the control-surface flutter derivatives of an NACA 65(sub 1)-213 airfoil in the Ames 16-foot high-speed wind tunnel

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