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Computer and wind tunnel development of flaps and control surfaces for advanced technology general aviation airfoils

机译：用于先进技术通用航空翼型的襟翼和控制表面的计算机和风洞开发

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作者
Wentz, W. H., Jr.;
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年度 1975
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOILS; FLAPS (CONTROL SURFACES); WIND TUNNEL TESTS; COMPUTER AIDED DESIGN; GENERAL AVIATION AIRCRAFT;

机译：翼型; FLaps（控制表面）;风洞隧道测试;计算机辅助设计;一般航空飞机;

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专利

1. Comparative in-flight and wind tunnel investigation of the development of natural and controlled disturbances in the laminar boundary layer of an airfoil [J] . Inken Peltzer Experiments in Fluids . 2008,第6期

机译：机翼层流边界层中自然扰动和受控扰动发展的空中和风洞比较研究
2. Comparative in-flight and wind tunnel investigation of the development of natural and controlled disturbances in the laminar boundary layer of an airfoil [J] . Peltzer I Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2008,第6期

机译：机翼层流边界层中自然扰动和受控扰动发展的空中和风洞比较研究
3. Development, implementation, and testing of fault detection strategies on the National Wind Technology Center's controls advanced research turbines [J] . Kathryn E. Johnson, Paul A. Fleming Mechatronics: The Science of Intelligent Machines . 2011,第4期

机译：在国家风力技术中心控制先进研究型涡轮机上开发，实施和测试故障检测策略
4. Dust Wind Tunnels Computer Fuzzy Control Spraying System Based On OpenGL Technology [C] . Ke Li, Wangkai Liu, Wei Lan, ICCCI 2010;International conference on computer and computational intelligence . 2010

机译：基于OpenGL技术的粉尘风洞计算机模糊控制喷涂系统。
5. Wind tunnel test of a tailless aircraft with a belly-flap control surface used in combination with wing flaps. [D] . Dougherty, Daniel A. 2012

机译：带有襟翼控制面并与机翼襟翼配合使用的无尾飞机的风洞测试。
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. Wind tunnel testing of an airfoil with a moving surface boundary-layer control. [O] . Al-Garni Abdullah Mohammed 1999

机译：具有移动表面边界层控制的翼型的风洞测试。
8. Wind tunnel investigation of control-surface characteristics XXIII : a 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil [R] . Spearman, M Leroy 1945

机译：控制表面特征的风洞调查XXIII：带有翼片的0.25翼型弦翼，翼片在NaCa 0009翼型上具有两倍的翼弦弦

Computer and wind tunnel development of flaps and control surfaces for advanced technology general aviation airfoils

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