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研究生: 方東
Phuong, Dong
論文名稱: 水滴翼型之阻力劇變現象實驗研究
AN EXPERIMENTAL STUDY ABOUT DRAG CRISIS PHENOMENON OF TEARDROP
指導教授: 苗君易
Miau, Jiun-Jih
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2018
畢業學年度: 106
語文別: 英文
論文頁數: 50
外文關鍵詞: drag crisis phenomenon, teardrop model, laminar separation bubble, transition
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  • We all know that drag plays a key role in our normal life when it acts opposite to the direction of movement of an object moving with respect to a surrounding fluid. It can be said that drag is the force prevents human reaching to new high levels, so finding ways to reduce drag are always the desires of many scientists, designers or athletes. Drag crisis is an interesting phenomenon in which an object experiences a sudden drop in drag coefficient at high Reynolds number while drag normally just increases with speed. Although this has been investigated well for some round bodies such as spheres and cylinders, airfoil objects which have better aerodynamic performances than cylinders or spheres are still not studied comprehensively about their drag crisis phenomenon.
    Teardrop which is a combination of a cylinder and a symmetry airfoil has been applied in bicycle frame and considered as frame revolution became a popular choice. Teardrop-sharping forms became a basis of nearly every bike at 2015 Tour de France because of its drag coefficient reduction advantages – teardrop drag coefficient could be just 1/20 of circular cylinder drag coefficient. Therefore, a comprehensive study about the drag crisis phenomenon of this kind of shape can provide the necessary knowledge to develop teardrop advantages in the future.
    Experiments were conducted on a teardrop model to investigate the phenomenon of drag crisis in wind tunnel in a range of Reynolds number 2 x 104 < Re < 8 x 104. Drag measurement experiment is carried out first in order to identify the Re range of the phenomenon with the angle of attack (AOA) = 0o. In addition, wake measurement and oil film results can provide further evidence about the critical regime when the drag crisis takes place. Then, results from the static pressure measurement experiment enable us to explore more about the characteristics of the laminar separation bubble (LSB) which is the main feature of the phenomenon. Drag crisis characteristics and its behaviors respecting to different AOA and roughness conditions are also investigated in this study.

    ACKNOWLEDGEMENTS II ABSTRACT III TABLE OF CONTENTS V LIST OF TABLES VII LIST OF FIGURES VIII CHAPTER ONE INTRODUCTION 1 1.1 Research Background. 1 1.1.1 Introduction. 1 1.1.2 Literature survey. 1 CHAPTER TWO EXPERIMENTS SET-UP 8 2.1 Airfoil geometry 8 2.2 Wind tunnel 10 2.3 Wind tunnel flow correction 11 2.4 Force balance 13 2.5 Pressure Transducer sensor 13 2.6 Hot-wire probes 14 2.7 Traversing system 15 2.8 Visual flow tools 15 CHAPTER THREE EXPERIMENTS APPROACH 17 3.1 Analysis of experimental parameters 17 3.1.1 Reynolds number 17 3.1.2 Pressure coefficient 17 3.1.3 Basic turbulence statistics 18 3.1.4 Non-dimensionalization factors 18 3.1.5 Drag coefficient and lift coefficient 19 3.2 Methods 19 3.2.1 Hot wire experiment 19 3.2.2 Drag measurement experiment 20 3.2.3 Pressure drag coefficient calculation 20 3.2.4 XFOIL program 22 3.2.5 Detached Eddy Simulation (DES) 23 CHAPTER FOUR RESEARCH RESULTS 25 4.1 Relation between drag crisis and critical regime 25 4.2 Relation between drag crisis and LSB 29 4.3 Relation between drag crisis and drag pressure coefficient 37 4.4 Drag crisis with changing AOA 41 4.5 Drag crisis with changing roughness height 42 CHAPTER FIVE CONCLUSIONS AND SUGGESTIONS 45 5.1 Conclusions 45 5.2 Suggestions 46 REFERENCES 47

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