Wind tunnel tests of the inverted joined wing and a comparison with CFD results

Galinski Cezary; Krysztofiak Grzegorz; Miller Marek; Ruchala Pawel; Kalski Marek; Lis Mateusz; Dziubinski Adam; Bogdanski Krzysztof; Stefanek Lukasz; Hajduk Jaroslaw

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Wind tunnel tests of the inverted joined wing and a comparison with CFD results

机译：倒置连接机翼的风洞试验及其与CFD结果的比较

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摘要

Purpose The purpose of this paper is to present the methodology and approach adapted to conduct a wind tunnel experiment on the inverted joined-wing airplane flying model together with the results obtained.

机译：目的本文的目的是介绍适用于在倒置联合翼飞机飞行模型上进行风洞实验的方法和方法，以及获得的结果。

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来源
《Aircraft engineering》 |2018年第4期|586-601|共16页
作者
Galinski Cezary; Krysztofiak Grzegorz; Miller Marek; Ruchala Pawel; Kalski Marek; Lis Mateusz; Dziubinski Adam; Bogdanski Krzysztof; Stefanek Lukasz; Hajduk Jaroslaw;
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作者单位

Ctr New Technol, Inst Aviat, Dept Aerodynam, Warsaw, Poland;

Ctr New Technol, Inst Aviat, Dept Aerodynam, Warsaw, Poland;

Ctr New Technol, Inst Aviat, Dept Aerodynam, Warsaw, Poland;

Ctr New Technol, Inst Aviat, Dept Aerodynam, Warsaw, Poland;

Ctr New Technol, Inst Aviat, Dept Aerodynam, Warsaw, Poland;

EDC Warsaw, GE, Aviat Syst, Warsaw, Poland;

Ctr New Technol, Inst Aviat, Dept Aerodynam, Warsaw, Poland;

Warsaw Univ Technol, Div Airplanes & Helicopters, Warsaw, Poland;

MSP, Design Off, Warsaw, Poland;

Air Force Inst Technol, Dept Airplanes & Helicopters, Warsaw, Poland;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Unmanned Air Vehicle (UAV); Joined wing; Wind tunnel tests;

机译：无人飞行器（UAV）;联翼;风洞测试;
入库时间 2022-08-18 02:23:57

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专利

1. Comparison of wind pressure measurements on tower-like structure obtained from full-scale observation, wind tunnel test, and the CFD technology [J] . Morimasa Watakabe, Masamiki Ohashi, Hisashi Okada, Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2002,第12a15期

机译：通过全面观测，风洞测试和CFD技术获得的塔状结构上的风压测量结果的比较
2. Joined-Wing Wind-Tunnel Test for Longitudinal Control via Aftwing Twist [J] . Vanessa L. Bond Journal of Aircraft . 2010,第5期

机译：通过机翼扭转进行纵向控制的联合翼风洞试验
3. Joined-Wing Wind-Tunnel Test for Longitudinal Control via Aftwing Twist [J] . Vanessa L. Bond, rnRobert A. Canfield, rnMaria da Luz Madruga Santos Matos, Journal of Aircraft . 2010,第5期

机译：通过机翼扭转进行纵向控制的联合翼风洞试验
4. Wind Tunnel Testing of a Twisted Wing for Longitudinal Control in a Joined- Wing Aircraft [C] . V. Bond, R. Canfield, M. Madruga, AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference . 2007

机译：联合机翼中用于纵向控制的扭曲机翼的风洞测试
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. 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. Aeroservoelastic Wind-Tunnel Tests of a Free-Flying, Joined-Wing SensorCraft Model for Gust Load Alleviation [O] . Castelluccio Mark A., Coulson David A., Heeg Jennifer, 2011

机译：自由飞行，联队翼SensorCraft模型的航空气动弹性风洞试验，用于减轻阵风载荷
8. Tests in the R.A.E. Io-ft x 7-ft High Speed Wind Tunnel on Drop Tanks fitted to Two Swept-Back Wings PARTSⅠComparison of Under-Wing and Wing-Tip Installations PARTⅡComparison of Various Under-Wing Drop-Tank Arrangements [R] . D. E. HARTLEY, A. B. HAINES 1956

机译：R.a.E.的测试安装在两个后掠翼上的水箱上的Io-ft x 7英尺高速风洞paRTsⅠ下翼和翼尖装置的比较paRTⅡ各种下翼下水箱布置的比较

Wind tunnel tests of the inverted joined wing and a comparison with CFD results

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