簡易檢索 / 詳目顯示

研究生: 左雷丹
Zoghlami, Alaeddine
論文名稱: 粗糙度對水滴翼型流場的影響
Effect Of The Roughness On Flow Over A Teardrop Model
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: 2019
畢業學年度: 107
語文別: 英文
論文頁數: 51
外文關鍵詞: teardrop model, textile roughness, drag crisis, laminar separation bubble, critical transition
相關次數: 點閱:61下載:0
分享至:
查詢本校圖書館目錄 查詢臺灣博碩士論文知識加值系統 勘誤回報
  • Aerodynamics is the study of moving of fluids, mainly air flows, and its possible effects on the motion of surrounding solid objects. It qualifies the appearance of a moving body in the air and its resistance to advancement. It is not a terminology limited to the phenomena occurring in aviation but present everywhere in our daily life. It can be found not only in vehicles (e.g. automobiles, bicycles, railways) and building and construction (e.g. skyscrapers, bridges), but also in propulsion systems (e.g. propellers, rotors, turbines, reactors) and renewable energy production (e.g. wind turbines).
    Since the dawn of time, humans have sought to create, invent and improve tools and techniques that are vital for survival. With the advancement of technology, the quest for competitivity and ecology lead the scientists to find the best parameter that can enhance the performance of current apparatus.
    The drag is the impedance that prevents humans from reaching optimal performance and thus is often studied to ameliorate its negative effects. Athletes, designers and scientists are all unanimous on devising means to break world records, to be more efficient or even to become more ecological by reducing drag.
    In fluid dynamics, drag crisis or Eiffel Paradox of a two- or three-dimensional object is a very counterintuitive phenomenon where the drag coefficient of the body decreases drastically while the velocity of flow increases. This phenomenon has been investigated using the models of simple shapes such as spheres and cylinders.
    Unfortunately, sometimes many parameters are given and cannot be changed. this is how the roughness makes its entrance. Scientists have already shown in the past that roughness can be beneficial on bluff body to a given Reynolds number range.
    In the current research, a teardrop-shaped foil which is a combination of a cylinder and a symmetry airfoil was used in a range of Reynolds number 3 x 104 < Re < 8 x 104. All the experiments were carried out at the National Cheng Kung University (NCKU, Taiwan) in an open jet tunnel. Initially, a drag measurement experiment identified the Re range of the phenomenon with the angle of attack (AOA) = 0°.
    The investigation has been done with three different cases (smooth teardrop and two different sample) to study the effect of textile roughness on the aerodynamic flow around the teardrop. The first one was the investigation of drag-lift and mean pressure over a smooth teardrop. Subsequently, the same experiment was conducted with the teardrop wrapped with two different samples of textile. A laser scanning microscope has been also used to determine the roughness of each textile sample.

    TABLE OF CONTENTS ABSTRACT II ACKNOWLEDGEMENTS V TABLE OF CONTENTS VI LIST OF TABLES IX LIST OF FIGURES X NOMENCLATURE 1 CHAPTER ONE INTRODUCTION 3 1.1 General Introduction 3 1.2 Previous and Related Studies 4 CHAPTER TWO EXPERIMENTS SET-UP 10 2.1 Software 10 2.1.1 SolidWorks 10 2.1.2 Xflr5 11 2.1.3 LabVIEW 12 2.1.4 MATLAB 12 2.2 Open jet wind tunnel 13 2.3 Teardrop model geometry 14 2.4 Pitot tube and Pressure transducer 16 2.5 Force balance 18 2.6 Pressure Transducer sensor 19 2.7 Hot-wire probes 19 2.8 Laser scanning microscope 20 2.9 Data Acquisition System 21 2.10 Flow chart 22 2.10.1 Drag-Lift 22 2.10.2 Pressure measurement 22 CHAPTER THREE EXPERIMENTS METHOD 23 3.1 Analysis of experimental parameters 23 3.1.1 Drag-Lift coefficient and Reynolds number 23 3.1.2 Pressure coefficient 24 3.1.3 Turbulence statistics 24 3.2 Roughness analyze 25 3.3 Methods 26 3.3.1 Hot wire experiment 26 3.3.3 Pressure drag coefficient calculation 26 CHAPTER FOUR RESEARCH RESULTS 28 4.1 Verification of the flow 28 4.2 Textile measurement 29 4.2.1 Sample A 29 4.2.1 Sample B 29 4.3 Drag coefficient with three cases 30 4.4 Lift coefficient with three cases 31 4.5 Xflr5 results and comparison 32 4.6 Laminar Separation Bubble 33 4.6.1 Smooth teardrop 34 4.6.2 Teardrop with sample A 37 4.6.3 Teardrop with sample B 40 CHAPTER FIVE CONCLUSIONS AND SUGGESTIONS 46 5.1 Conclusions 46 5.2 Future work 48 REFERENCES 49

    ACHENBACH, E (1968) Distribution of local pressure and skin friction around a circular cylinder in cross-flow up to Re = 5 × 106 , J. Fluid Mech., vol. 34, pp. 625–639.
    ACHENBACH, E. (1971) Influence of surface roughness on the cross-flow around a circular cylinder, J. Fluid Mech., vol. 46, pp. 321–335.
    AHOLT, J. & FINAISH, F. (2011) Active Flow control Strategy of Laminar Separation Bubbles Developed over Subsonic Airfoils at Low Reynolds Numbers AIAA 2011-733
    BEARMAN, P.W. (1969) On vortex shedding from a circular cylinder in the critical Reynolds number regime, J. Fluid Mech, vol. 37, pp. 511-585.
    CHANETZ B. (2017) Comptes Rendus Mécanique Volume 345, Issue 8, August 2017, Pages 581-594
    CHARKROUN A., (2004) Effect of Surface Roughness on the Aerodynamic Characteristics of a Symmetrical Airfoil. Wind engineering volume 28, no. 5, 2004 PP 547–564
    CHOPRA. G, MITTAL. S. (2017) The intermittent nature of the laminar separation bubble on a cylinder in uniform flow, Computers & Fluids, vol. 142, pp. 118-127.
    CLIFT R. , GRACE J.R. AND WEBER M.E. (1978) Drops, And Particles, Bubbles, Drops, And Particles.
    DESHPANDE. R, KANTI. V, DESAI. A, MITTAL. S. (2017) Intermittency of laminar separation bubble on a sphere during drag crisis, Journal of Fluid Mech., vol. 812, pp. 815-840.
    DONGLI M., YANPING Z., YUHANG Q. & GUANXIONG L. (2015) Effects of relative thickness on aerodynamic characteristics of airfoil at a low Reynolds number, Chinese Journal of Aeronautics, vol. 28, no. 4, pp. 1003-1015.
    DYKE, M. V, (1982) An Album of Fluid Motion, 4th edition, the Parabolic Press, pp. 34-35.
    EIFFEL G. (1914) Nouvelles recherches sur la résistance de l’air et l’aviation faites au laboratoire d’Auteuil H. Dunot et E. Pinat, éditeurs.
    HORTON H. P., (1968) Laminar separation bubbles in two- and three-dimensional incompressible flow Ph.D. dissertation University of London.
    MASTENBROEK J.J. (2010) Bluff body flow wake behavior behind a heated circular cylinder university of Twente.
    MIAU, J. J., LAI, Y. H., TSAI, Z. X., HSU, X. Y., & CIOU, Y. S. (2016) The effect of textile roughness on the critical transition of flow over a circular cylinder In The 14th Asian Symposium on Visualization, Beijing, China.
    MIAU, J. J., WONG, H., and HUSSON, S., 2014 2D CFD study of cross-section foils performances in cycling aerodynamics, 16th International Symposium on Flow Visualization June 24-28, 2014, Okinawa, Japan.
    Ni.com. (2015). LabVIEW for ECG Signal Processing - National Instruments http://www.ni.com/tutorial/6349/en/
    NI 9215 Datasheet by National Instrument (2016)
    http://www.ni.com/pdf/manuals/373779a_02.pdf
    OWEN, P. R. & KLANFER, L. (1953) On the laminar boundary layer separation from the leading edge of a thin aerofoil. RAE Rep. Aero. 2508.
    PHUONG DONG, MIAU J.J, (2018) An experiment study about drag crisis phenomenon on teardrop model AASRC Conference Tainan, Taiwan.
    PRANDTL, L. (1914) Nachr. Ges. Wiss. Gottingen, Math-phys. KI., pp. 177-190.
    PRANDTL L., (1927) NACA Technical Memorandum No. 452 : “Notion Of Fluids With Very Little Viscosity, NACA
    QIANG L., FENG B., FENG L. (2017) Aerodynamic characteristics of airfoil and evolution of laminar separation at different Reynolds numbers, ACTA Aeronauticaet Astronautica Sinica, vol. 38, no. 4, pp. 120338-120338.
    REYNOLDS O. (1883) An experimental investigation of the circumstances which determine whether the motion of water in parallel channels shall be direct or sinuous and of the law of resistance in parallel channels. Philosophical Transactions of the Royal Society of London, Vol. 174 (1883), pp. 935-982
    ROSHKO, A. (1961) Experiments on the flow past a circular cylinder at very high Reynolds number Journal of Fluid Mech., vol. 10, pp. 345-356.
    TANI, I. (1964) Low-speed flows involving bubble separations. Prog. Aero. Sci, vol. 5, pp. 70–103.
    WILLIAMSON, C. H. K (1996). Vortex dynamics in the cylinder wake, Annu. Rev, Fluid Mech., vol. 28, pp. 477–539.
    WONG H., J. J. MIAU, 2015 Flow separation control with a truncated ellipse airfoil in cycling aerodynamics, The 13th Asian symposium on visualization, 22-26 June, 2015, Novosibirsk, Russia.
    ZDRAVKOVISCH. (1977) A Review on the Study of Wind Loads on Multiple Cylinders with Effects of Turbulence and Surface Roughness.
    ZHOU Y. AND WANG Z. J. (2011) Effects of surface roughness on laminar separation bubble over a wing at a low-Reynolds number AIAA Paper No. 2011-0736, 2011.

    無法下載圖示 校內:2024-07-19公開
    校外:不公開
    電子論文尚未授權公開,紙本請查館藏目錄
    QR CODE