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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

机译：优化和设计飞机变形翼尖演示器，用于低速减阻，第II部分 - 使用风洞试验的红外转换测量进行的实验验证

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Andreea Koreanschi; Oliviu Sugar Gabor; Joran Acotto; Guillaume Brianchon; Gregoire Portier; Ruxandra Mihaela Botez; Mahmoud Mamou; Youssef Mebarki;
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年度 2017
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入库时间 2022-08-20 21:17:28

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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. Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speed, Part Ⅰ–Aerodynamic optimization using genetic, bee colony and gradient descent algorithms [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，第一部分–使用遗传，蜂群和梯度下降算法进行空气动力学优化
3. Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance [J] . Gabor Oliviu Sugar, Koreanschi Andreea, Botez Ruxandra Mihaela, Aerospace science and technology . 2016,第Juna期

机译：变形翼尖演示器气动性能的数值模拟和风洞试验研究与验证
4. Computational and Experimental Investigation of Camber Morphing Airfoils for Reverse Flow Drag Reduction on High-Speed Rotorcraft [C] . George Jacobellis, Farhan Gandhi, Thomas Rice, Annual AHS international forum and technology display . 2018

机译：高速旋翼机上用于降低逆流阻力的弧形翼型的计算和实验研究
5. Numerical and Experimental Validation of the Optimization Methodologies for a Wing-Tip Structure Equipped with Conventional and Morphing Ailerons = [D] . Koreanschi, Andreea. 2016

机译：配备常规和变形副翼的翼尖结构优化方法的数值和实验验证=
6. Fuzzy Logic-Based Control for a Morphing Wing Tip Actuation System: Design Numerical Simulation and Wind Tunnel Experimental Testing [O] . Shehryar Khan, Teodor Lucian Grigorie, Ruxandra Mihaela Botez, 2019

机译：变形翼尖驱动系统的基于模糊逻辑的控制：设计数值模拟和风洞实验测试
7. 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 [O] . Koreanschi A, Sugar-Gabor O, Acotto J, 2017

机译：优化和设计用于降低低速阻力的飞机变形翼尖演示器，第二部分-使用来自风洞测试的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

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

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