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Some effects of Reynolds and Mach numbers on the lift of an NACA 0012 rectangular wing in the NACA 19-foot pressure tunnel

机译：雷诺和马赫数对NaCa 19英尺压力隧道中NaCa 0012矩形机翼升力的影响

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Muse, Thomas C;
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年度 1943
页码 1-11
总页数 11
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LIFT COEFFICIENTS - AIRFOILS - NACA 0012; AIR FLOW - COMPRESSIBILITY; REYNOLDS NUMBER; MACH NUMBER; WINGS, RECTANGULAR - CHARACTERISTICS; WIND TUNNEL TESTS - NACA - PRESSURE (19');

机译：提升系数 - 翼型 - NaCa 0012;空气流动 - 可压缩性; REYNOLDs NUmBER;马赫数; WINGs，RECTaNGULaR - CHaRaCTERIsTICs;风洞隧道测试 - NaCa - 压力（19'）;

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1. Effect of the Reynolds Number on the Performance of a NACA0012 Wing with Leading Edge Protuberance at Low Reynolds Numbers [J] . Yasuda Takahiro, Fukui Keita, Matsuo Keiji, Flow, turbulence and combustion . 2019,第2期

机译：雷诺数对NACA0012翼的效果在低雷诺数下具有前缘突起的效果
2. 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
3. Reynolds-Averaged Navier-Stokes Simulations on NACA0012 and ONERA-M6 Wing with the ONERA elsA Solver [J] . Mayeur J., Dumont A., Destarac D., AIAA Journal . 2016,第9期

机译：使用ONERA elsA解算器在NACA0012和ONERA-M6机翼上进行雷诺平均Navier-Stokes模拟
4. A Comparison of NACA 0012 and NACA 0021 Self-noise at Low Reynolds Number [C] . A. Laratro, M. Arjomandi, B. Cazzolato, Symposium on Fluid-Structure-Sound Interactions and Control . 2016

机译：NaCA 0012和NaCA 0021在低雷诺数下的自噪声的比较
5. Investigation of the Ground Effect on Wingtip Vortex Generated by a Rectangular NACA0012 Wing [D] . Lu, Anan. 2020

机译：矩形Naca0012翼生成的Wingtip Vortex的基础影响研究
6. On the lift-optimal aspect ratio of a revolving wing at low Reynolds number [O] . T. Jardin, T. Colonius 2018

机译：低雷诺数下旋转翼升力最佳纵横比
7. Dynamics Of A Free Pitching Flexible Cantilever Naca0012 Airfoil At Transitional Reynolds Numbers [O] . Crystal Itwar Barrett, Dominique Poirel 2018

机译：在过渡雷诺数下的自由俯仰柔性悬臂翼型的动态
8. Some Effects of Reynolds and Mach Numbers on the Lift of an NACA 0012 Rectangular Wing in the NACA 19-Foot Pressure Tunnel [R] . Muse, T C 1943

机译：雷诺兹和马赫数上的NaCa 0012矩形翼在NaCa 19脚压力隧道升降机的某些影响

Some effects of Reynolds and Mach numbers on the lift of an NACA 0012 rectangular wing in the NACA 19-foot pressure tunnel

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