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Development of a Morphing Aircraft Model for Wind Tunnel Experimentation

机译：用于风洞实验的变形飞机模型的开发

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《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference》|2006年|P.1-14|共14页
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D. Neal; J. Farmer; D. Inman;
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中图分类流体动力学;
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1. Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speeds, Part Ⅱ-Experimental validation using Infra-Red transition measurement from Wind Tunnel tests [J] . Andreea Koreanschi, Oliviu Sugar Gabor, Joran Acotto, 中国航空学报（英文版） . 2017,第001期

机译：用于低速降低阻力的飞机变形翼尖演示器的优化和设计，第二部分-使用风洞试验的红外过渡测量进行实验验证
2. Development of a Technique and Method of Testing Aircraft Models with Turboprop Engine Simulators in a Small-scale Wind Tunnel - Results of Tests [J] . A. V. Petrov, M. V. Shmakov, Y. G. Stepanov Acta polytechnica . 2004,第2期

机译：在小型风洞中使用涡轮螺旋桨发动机模拟器测试飞机模型的技术和方法的开发-测试结果
3. Development of a Technique and Method of Testing Aircraft Models with Turboprop Engine Simulators in a Small-scale Wind Tunnel - Results of Tests [J] . A. V. Petrov, Y. G. Stepanov, M. V. Shmakov Acta Polytechnica . 2004,第2期

机译：在小型风洞中使用涡轮螺旋桨发动机模拟器测试飞机模型的技术和方法的开发-测试结果
4. Development of a Morphing Aircraft Model for Wind Tunnel Experimentation [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/American Helicopter Society/ASC Structures, Structural Dynamics, and Materials Conference . 2006

机译：风洞实验传感飞机模型的发展
5. Design, Development and Tests in Real Time of Control Methodologies for a Morphing Wing in Wind Tunnel = [D] . Tchatchueng Kammegne, Michel Joel. 2016

机译：风洞中变形翼的控制方法的实时设计，开发和测试=
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. Optimization and design of a morphing wing tip aircraft demonstrator for drag reduction at low speeds, Part II \u2013 Experimental validation using infra-red transition measurements during wind tunnel tests [O] . Koreanschi, Andreea, Gabor, Oliviu Sugar, Acotto, Joran, 2017

机译：优化和设计用于降低低速风阻的变形翼尖飞机演示器，第二部分\ u2013在风洞测试期间使用红外过渡测量进行实验验证
8. Wind-tunnel Tests on an Aircraft Designed for Supersonic Speeds PART I High-speed Wind-tunnel Tests on 1/6.15-Scale Model Aircraft PART II No. 2 II1/2 -ft. Wind-tunnel Tests on a 1/4-Scale Model Wing [R] . S. P. HUTTON, M. Eng., A. D. Young 1950

机译：针对超音速设计的飞机的风洞测试第一部分1 / 6.15比例模型飞机的高速风洞试验第II部分第2号II1 / 2英尺。风洞测试1/4比例模型翼

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