Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System

碩士 === 國立彰化師範大學 === 機電工程學系 === 106 === The use of micro aerial vehicles (MAV) has become a rapidly growing class of aerial vehicle for habit, commercial, industrial and many other applications. However, micro aerial vehicle design is a challenge because of the lack of understanding about the aerodyn...

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Main Authors: Hsu, An-Yu, 徐安裕
Other Authors: Wang, Ker-win
Format: Others
Language:zh-TW
Published: 2018
Online Access:http://ndltd.ncl.edu.tw/handle/48b4p2
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spelling ndltd-TW-106NCUE54890112019-05-30T03:57:13Z http://ndltd.ncl.edu.tw/handle/48b4p2 Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System 仿生串列可變翼空氣動力學特性的實驗調查與優化 Hsu, An-Yu 徐安裕 碩士 國立彰化師範大學 機電工程學系 106 The use of micro aerial vehicles (MAV) has become a rapidly growing class of aerial vehicle for habit, commercial, industrial and many other applications. However, micro aerial vehicle design is a challenge because of the lack of understanding about the aerodynamics of miniaturized aircraft at low speeds. This paper presents a novel tandem-morphing wing system for MAV design. The bio-inspired design is tested with various angles of attack for low chord Reynolds number regime. 16 different morphing-wing configurations are tested for lift-to-drag ratio optimization. These systematic experiments link the influence of the airfoil configurations of tandem-morphing wings to its aerodynamic performance. Wang, Ker-win 王可文 2018 學位論文 ; thesis 133 zh-TW
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language zh-TW
format Others
sources NDLTD
description 碩士 === 國立彰化師範大學 === 機電工程學系 === 106 === The use of micro aerial vehicles (MAV) has become a rapidly growing class of aerial vehicle for habit, commercial, industrial and many other applications. However, micro aerial vehicle design is a challenge because of the lack of understanding about the aerodynamics of miniaturized aircraft at low speeds. This paper presents a novel tandem-morphing wing system for MAV design. The bio-inspired design is tested with various angles of attack for low chord Reynolds number regime. 16 different morphing-wing configurations are tested for lift-to-drag ratio optimization. These systematic experiments link the influence of the airfoil configurations of tandem-morphing wings to its aerodynamic performance.
author2 Wang, Ker-win
author_facet Wang, Ker-win
Hsu, An-Yu
徐安裕
author Hsu, An-Yu
徐安裕
spellingShingle Hsu, An-Yu
徐安裕
Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System
author_sort Hsu, An-Yu
title Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System
title_short Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System
title_full Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System
title_fullStr Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System
title_full_unstemmed Experimental Investigation and Optimization on the Aerodynamic Characteristics of a Biomimetic Morphing Tandem-Wing System
title_sort experimental investigation and optimization on the aerodynamic characteristics of a biomimetic morphing tandem-wing system
publishDate 2018
url http://ndltd.ncl.edu.tw/handle/48b4p2
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