DRAG REDUCTION IN DUCTS USING STRUCTURED INTERNAL SURFACES

Transcription

1 DRAG REDUCTION IN DUCTS USING STRUCTURED INTERNAL SURFACES HASSAN DHIAALDEEN MAHAMMED AL-HASHEM DOCTOR OF PHILOSOPHY UNIVERSITI MALAYSIA PAHANG

2 SUPERVISOR S DECLARATION I hereby declare that I have checked this thesis and in my opinion, this thesis is adequate in terms of scope and quality for the award of the degree of Doctor of Philosophy in chemical engineering. (Supervisor s Signature) Full Name : PROFESSOR DR. HAYDER A. ABDULBARI Position : PROFESSOR Date :

3 STUDENT S DECLARATION I hereby declare that the work in this thesis is based on my original work except for quotations and citations which have been duly acknowledged. I also declare that it has not been previously or concurrently submitted for any other degree at Universiti Malaysia Pahang or any other institutions. (Student s Signature) Full Name : HASSAN DHIAALDEEN MAHAMMED AL-HASHEM ID Number : PKC13011 Date :

4 DRAG REDUCTION IN DUCTS USING STRUCTURED INTERNAL SURFACES HASSAN DHIAALDEEN MAHAMMED AL-HASHEM Thesis submitted in fulfillment of the requirements for the award of the degree of Doctor of Philosophy Faculty of Chemical & Natural Resources Engineering UNIVERSITI MALAYSIA PAHANG FEBRUARY 2017

5 DEDICATION To My Dear Mother and Father In Recognition of Their Worth, Love, and Respect This Thesis Dedicated to the Memory of My Best Friend, Dr. Hayder Al-Safar May He Rest in Peace

6 ACKNOWLEDGEMENTS First of all, I want to thank God for giving me the strength and perseverance to complete this study. I would like to express my sincere gratitude to my advisors Asst. Prof. Dr. Hayder A. Abdulbari and Prof. Dr. Zulkefli Bin Yaacob for the continuous support of my PhD study and related research, for their patience, motivation, and immense knowledge. Their guidance, encouragement, and transmitted knowledge helped me in all the time of research and writing this thesis. I could not have imagined having better advisors for my PhD study. My respectful regards to the Dean of Chemical Engineering Faculty at University Malaysia Pahang PM. Zulkafli Bin Hassan for his kind help in providing facilities. I would like to convey my sincere appreciation to all Staff of Chemical Engineering Faculty. Last but not the least, I would like to thank Hussein Ali, who as a good friend, was always willing to help and give his best suggestions. It would have been a lonely life without him. I will never be able to thank Dr. Wafaa K. Mahmood, Wafaa Abd and Ateaf Khaled, Zainab Nazar Wafi, Abdul Rahman Riza, Steven Taniselass, enough for their help, support and for wise idea throughout the research. My research would not have been possible without their helps. Finally, I would like to thank my family: my parents and to my brother and sisters for supporting me spiritually throughout writing this thesis and my life in general. Hassan Dhiaaldeen Mahammed. Al-Hashem ii

7 ABSTRAK Menambahbaikkan aliran permukaan tenggelam seperti di dalam saluran paip, kapal selam, dan kapal terbang telah menarik minat ramai penyelidik sejak beberapa dekad yang lalu. Banyak tenaga yang telah digunakan untuk menangani daya seretan yang kebanyakannya mengakibatkan kehilangan tenaga. Beberapa teknik telah dijalankan untuk mencari jalan yang sesuai bagi menambahbaik aliran bagi permukaan tenggelam Terkini, kaedah yang paling popular untuk mengurangkan seretan ialah penggunaan aditif kaedah aktif. Walaubagaimanapun, kesemua kaedah aktif ini ada keburukannya seperti degradasi mekanikal, perubahan sifat kimia dan fizikal cecair serta menjadi toksik dan sebahagiannya tidak boleh terurai secara semulajadi dan banyak peringkat tambahan yang perlu dilakukan untuk memastikan aditif itu sesuai. Ini menyebabkan penambahan kos seiring dengan aditif tersebut. Hal ini telah membawa kepada penyelidikan baru yang lebih mesra alam dan pengurangan daya seretan yang tidak melibatkan aditif. Dalam kajian terbaru, dua set riblet direkabentuk dan dipalsukan. Setset tersebut diklasifikasikan berdasarkan alur mengikut orientasi (membujur dan melintang). Riblet kedua-dua set mengandungi lima subset dari lima bentuk riblet (segi tiga, trapezoid, segi tiga djarakkan, alur-l, dan alur-i). Setiap bentuk riblet mempunyai ketinggian 600, 800, dan 1000 μm dengan jarak yang berlainan supaya daya paduan ke arah aliran kekal sama. Hal ini bagi menyediakan perbandingan yang tepat pada kesan riblet ke arah aliran bergelora di dalam sistem aliran tertutup dengan keadaan operasi yang berbeza. Pengagihan halaju ke atas permukaan yang dikaji ditentukan menggunakan system mini-ldv. Data eksperimen menunjukkan peratusan pengurangan seretan (%DR) adalah lebih tinggi dan lebih efisyen apabila arah aliran permukaan berstruktur ialah membujur. Menambahkan ketinggian riblet akan menyebabkan penurunan %DR. Keputusan ujikaji menunjukkan riblet alur-u mempunyai %DR yang tertinggi dengan penambahbaikan aliran maksimum sebanyak 13.7% dilihat pada reka bentuk 600 x 750 µm. Ukuran penurunan daya tekanan pada kerja ini memberikan indikasi yang jelas serta pemetaan sifat aliran ke atas permukaan yang dikaji, dimana pengurangan dalam bacaan daya tekanan dikesan dengan tempoh masa yang hampir konsisten. Ini merupakan indikasi yang jelas tentang ciptaan dan pemecahan struktur bergelora ke atas permukaan apabila struktur permukaan itu berubah. Pengagihan halaju mini-ldv mendedahkan fakta bahawa sifat aliran ke atas permukaan rib berubah sepenuhnya apabila dibandingkan dengan permukaan licin. Nilai halaju permukaan rib adalah lebih rendah daripada permukaan licin apabila ukuran laser ialah 1 mm daripada arah permukaan dan ianya menjadi lebih tinggi berbanding nilai permukaan licin apabila ia mencapai titik ukuran maksimum (25 mm di atas permukaan). Dapatan yang sebegitu menyokong idea untuk mengubah arah gelora itu ke arah tengah salur di mana tahap pergolakan menjadi lebih tinggi. Kesimpulannya, didapati bahawa dimensi geometri boleh mengawal kesan pengurangan daya seretan walaupun arah aliran tersebut melintang dimana sebahagian kesan pengurangan daya seretan dilihat. iii

8 ABSTRACT Enhancing the flow of submerged surfaces as in pipeline, submarines, ships, and even airplanes attracted enormous numbers of researchers in the past few decades. A huge amount of energy has spent to overcome the drag force which results in a loss in energy. Several techniques were conducted to find the possible way to enhance the flow of submerged surfaces. Currently the most popular method for reducing drag employed the use of additives (active means). However, these active means do have drawbacks such as mechanical degradation, altering the chemical and physical properties of the fluid they inhabit as well as being toxic and non-biodegradable for the most part and many extra stages must be included to ensure that an additive is suitable. As a result, the additive increases costs and reverses savings. This has spurred new research aimed to explore more nature-friendly, non-additive means of drag reduction. In the present study, two sets of riblets we designed and fabricated, the sets classified according to groove according to orientations (longitudinal and transverse) riblets both sets contain five subsets of five riblet shapes (triangular, trapezoidal, spaced triangular, L-groove, and U-groove). Each riblet shape had heights of 600, 800 and 1000 μm, with varied spacing so that the resultant protrusions into the flow remained similar to provide an accurate comparison of the effects of riblets on turbulent flow in a closed loop channel flow system with different operating conditions. The velocity distribution over the investigated surfaces was determined using mini-ldv system. The experimental data showed that the percentage drag reduction (%DR) was higher and more efficient when the direction of flow over the structured surfaces is longitudinal. Increasing the riblets height led to a decrease in the %DR reported. The experimental results showed that the U-groove riblets had the highest %DR values with maximum flow enhancement of 13.7% observed in µm design. The pressure drop measurements of the present work gave a clear indication and mapping of the flow behavior over the investigated surfaces, where reductions in the pressure drop readings are spotted with almost consistent time periods and that is a clear indication of the creation and bursting of turbulence structures over the surfaces when the structure of the surface is changed. The mini-ldv velocity distribution reveals the fact that the flow behavior over the rib surfaces changes completely when compared to the smooth surface. The velocity values of the rib surfaces were lower than that of the smooth surfaces when the laser measurements were 1 mm from the surface, and it became much higher than the values of the smooth surfaces when it reaches its maximum measurement point (25 mm above the surface). Such finding supports the idea of redirecting the turbulence towards the center of the duct where the degree of turbulence became higher. Finally as a conclusion, it was found that the geometry dimensions can massively control the drag reduction effect even if the direction of flow is transverse where certain drag reduction effects can be measured. iv

9 TABLE OF CONTENT DECLARATION TITLE PAGE ACKNOWLEDGEMENTS ABSTRAK ABSTRACT TABLE OF CONTENT LIST OF TABLES LIST OF FIGURES LIST OF SYMBOLS LIST OF ABBREVIATIONS ii iii iv v ix x xiv xv CHAPTER 1 INTRODUCTION Background Riblets in Turbulent Flows Modification of Turbulence Structures and Mean Flows by Riblets Problem Statement Research Objectives Scope of Research Significance of the Study Thesis Organization 12 CHAPTER 2 LITERATURE REVIEW Introduction 13 v

10 2.2 Turbulent Flow Turbulence Control Foreign-Substance Drag Reduction Techniques (Active Means) Non-Additive Drag Reduction Techniques (Passive Means) Large Eddy Breakup Devices (LEBU) Compliant Coatings Dimples Oscillating walls Riblet grooves First Inspirations from Nature Mechanism Underlying Skin Friction Reduction Using Riblets Experimental Investigations of Riblets in Channels Riblets in Air Flows Riblets in Liquid Flows Drag Characteristics of Longitudinal and Transverse Riblets Summary 58 CHAPTER 3 RESEARCH METHODOLOGY Riblet Design and Fabrication Design Riblets Fabrication of the Ribbed Surfaces Experimental Facility and Instrumentation The Duct Flow System Instrumentation and Data Acquisition Variables Tested with Groove Riblets Pressure Drop Measurements 73 vi

11 3.5 Velocity Measurements Experimental Calculations Drag Reduction Percentage Velocity and Reynolds Number Friction Factor Non-Dimensional Groove Factor 80 CHAPTER 4 RESULTS AND DISCUSSION Verification of Experimental Data Effect of Groove Riblets on Degree of Turbulence Pressure Drop over Smooth and Ribbed Surfaces Effect of Reynolds Number on the Smooth and Ribbed Surfaces Effect of the Groove Riblet Orientation on Drag Reduction Influence of the Groove Orientation on the Resistance Factor Influence of Groove Orientation on the Percentage of Drag Reduction Effects of Groove Geometry on Drag Reduction Effect of the Groove Height Effect of the Groove Height to Spacing Ratio (h/s) Effect of the Groove Shape Time Series Analysis of Pressure Fluctuations across Smooth and Ribbed Surfaces Detection of Singularities in Pressure Drop Fluctuations over Smooth and Ribbed Surfaces Energy Dissipation Velocity Distribution and Mechanism Summary 139 vii

12 CHAPTER 5 CONCLUSION Introduction Conclusion Future Work 142 REFERENCES 143 APPENDIX A Test Facility Drawings 173 APPENDIX B Pressure drop results 179 APPENDIX C Drag reduction percentage 189 APPENDIX D Results of calculations wall share stress ( ) 199 APPENDIX E Results of calculations skin friction coefficient 209 APPENDIX F Results of calculations non-dimensional groove height 219 APPENDIX G Results of calculations non-dimensional groove space 229 APPENDIX I List of Publications 239 viii

13 LIST OF TABLES Table 2.1 Riblet models tested by NASA 38 Table 2.2 Table 2.3 Table 2.4 List of experimental wind studies over flat plates with different types of riblets 41 List of experimental studies of water flowing over flat plates with riblets of different types 49 List of experimental studies conducted in oil on flat plates with different types of riblets. 54 Table 3.1 Dimensions of the fabricated triangular riblets used in this study 62 Table 3.2 Dimensions of the fabricated trapezoidal riblets used in this study 62 Table 3.3 Dimensions of the fabricated spaced triangular riblets used in this study 62 Table 3.4 Dimensions of the fabricated L-groove riblets used in this study 63 Table 3.5 Dimensions of the fabricated U-groove riblets used in this study 63 Table 3.7 Chemical composition of the material 64 ix

14 LIST OF FIGURES Figure 1.1 The dimensions of the grooves used in previous studies and the present study regardless of their shapes and the type of fluid where (h) is groove height and (s) is peak to peak groove spacing 9 Figure 2.1 Coherent structures in a turbulent boundary layer 17 Figure 2.2 Types of turbulence control methods 18 Figure 2.3 Parameters that control the drag reduction of (A) outer layer manipulators and (B) inner layer manipulators 22 Figure 2.4 Vertical LEBUs mounted on the flat plate surface. 24 Figure 2.5 Kramer's compliant coatings 25 Figure 2.6 Figure 2.7 Channel flow with multiple dimples on both walls, case B, fine grid simulation, Re=10, Conceptual model for a turbulent boundary layer over an oscillating wall 28 Figure 2.8 Examples of natural surface structures 30 Figure 2.9 Longitudinal and cross flow on a ribbed surface 34 Figure 2.10 Figure 2.11 Figure 2.12 Figure 2.13 Figure 2.14 Figure 2.15 Figure 2.16 Riblet mechanisms for increase and decrease drag: (A) s + =40, drag increase and (B) s + = 20, drag decrease 35 Rectangular and triangular ribbed surfaces tested by Walsh and Weinstein 42 Friction drag reduction for (1) triangular riblets (h=170 µm and s=250 µm), (2) a smooth plate, and (3) the geometry studied by Walsh and Lindemann. 43 Flow visualization images of streamwise vortices over a ribbed surface: (A) a drag-reducing configuration and (B) a drag-increasing configuration 46 Riblet configuration for (A) Miki et al. (2011) and (B) Sasamori et al. (2014). 48 Schematic of a streamwise vortex interacting with a ribbed surface via viscous effects 50 Direct drag data for two V-groove ribbed surfaces: (1) h/s=0.22 and h=0.25 mm and (2) h/s=1 and h=0.5 mm 52 Figure 3.1 The dimensions of all the tested plates 65 Figure 3.2 Picture of the Wire Electrical Discharge Machining (WEDM) 66 Figure 3.3 Shows one sample of final fabricated workpiece 67 Figure 3.4 Sinpo JVL 250 vision measuring machine 68 Figure 3.5 Riblets used in the experiments: (A) triangular, (B) trapezoidal, (C) spaced triangular, (D) L-groove, and (E) U-groove 68 x

15 Figure 3.6 Schematic diagram of the experimental apparatus 69 Figure 3.7 Schematic of the test section 70 Figure 3.8 Schematic of the transition ducts 70 Figure 3.9 Mechanism of mini-ldv probe 75 Figure 3.10 Shows a photograph of the system in action 76 Figure 3.11 Flowchart of the experimental work with the investigated riblets 78 Figure 4.1 Figure 4.2 Figure 4.3 Figure 4.4 Figure 4.5 Figure 4.6 Figure 4.7 Figure 4.8 Figure 4.9 Figure 4.10 Figure 4.11 Figure 4.12 Figure 4.13 Comparison of the friction factors for water flow in a channel over a smooth plate and plates containing selected longitudinal groove riblets with the Blasius, Hoye, and Virk correlations. 83 Comparison of the friction factors for water flow in a channel over a smooth plate and plates containing selected transverse groove riblets with the Blasius, Hoye, and Virk correlations 83 Comparison of the pressure drops across the smooth plate and plates with longitudinal groove riblets 85 Comparison of the pressure drops across the smooth plate and plates with transverse groove riblets 86 Effect of the Reynolds number on the percentage of drag reduction for selected longitudinal groove riblets 88 Effect of the Reynolds number on the percentage of drag reduction for transverse groove riblets 89 Groove riblet configurations: (A) groove riblets that are oriented longitudinally to the flow and (B) groove riblets that are oriented transversely to the flow 90 Resistance factor versus Reynolds number for triangular riblets with groove heights of 600 µm: (A) groove riblets oriented longitudinally to the flow direction and (B) groove riblets oriented transversely to the flow 92 The percentage of drag reduction versus the Reynolds number for triangular riblets with a groove height of 600 µm: (A) triangular groove riblets oriented longitudinally to the flow direction and (B) triangular groove riblets oriented transversely to the flow direction 95 The percentage of drag reduction versus the non-dimensional riblet height for a groove height of 600 µm 97 The percentage of drag reduction versus the non-dimensional riblet height for a groove height of 800 µm. 98 The percentage of drag reduction versus the non-dimensional riblet height for a groove height of 1000 µm 99 Percentage of drag reduction versus (A) Reynolds number and (B) for triangular groove riblets with a groove height of 600 µm and varying aspect ratios 101 xi

16 Figure 4.14 Figure 4.15 Figure 4.16 Figure 4.17 Figure 4.18 Figure 4.19 Figure 4.20 Figure 4.21 Figure 4.22 Figure 4.23 Figure 4.24 Figure 4.25 Percentage of drag reduction versus (A) Reynolds number and (B) for trapezoidal groove riblets with a groove height of 600 µm and varying aspect ratios. 103 Percentage of drag reduction versus (A) Reynolds number and (B) for L-groove riblets with a groove height of 600 µm and varying aspect ratios. 105 Percentage of drag reduction versus (A) Reynolds number and (B) of U-groove riblets with a groove height of 600 µm and varying aspect ratios. 106 Percentage of drag reduction versus (A) Reynolds number and (B) for spaced triangular groove riblets with a groove height of 600 µm and varying aspect ratios. 108 Effect of the groove shape on the pressure drop for dimensions of μm 110 Effect of the groove shape on the pressure drop for dimensions of μm 111 Effect of the groove shape on the pressure drop for dimensions of μm. 111 Effect the groove shape on the pressure drop for dimensions of μm. 112 Effect of time on the pressure drop across a smooth surface and selected triangular grooves at a Reynolds number of 116 Effect of time on the pressure drop across a smooth surface and selected trapezoidal grooves at a Reynolds number of 117 Effect of time on the pressure drop across a smooth surface and spaced triangular riblets at a Reynolds number of. 118 Effect of time on the pressure drop over a smooth surface and selected L-grooves at a Reynolds number of. 119 Figure 4.26 Effect of time on the pressure drop over a smooth and selected U- grooves at a Reynolds number of. 120 Figure 4.27 Figure 4.28 Pressure fluctuation time series for a Reynolds number of for a smooth surface and U-groove riblets 123 Profiles of the pressure fluctuation time series at different Reynolds numbers for a smooth surface and a surface covered with U-groove riblets with dimensions of 600 µm 750 µm. 125 Figure 4.29 Dissipation energy profile of selected triangular riblets 127 Figure 4.30 Dissipation energy profile of selected trapezoidal riblets 127 Figure 4.31 Dissipation energy profile of selected spaced triangular riblets 128 Figure 4.32 Dissipation energy profile of selected L-groove riblets 128 Figure 4.33 Dissipation energy profile of selected U-groove riblets 129 Figure 4.34 Velocity measurements over smooth and triangular rib surfaces 131 xii

17 Figure 4.35 Velocity measurements over smooth and trapezoidal rib surfaces 131 Figure 4.36 Velocity measurements over smooth and spaced triangular rib surfaces 132 Figure 4.37 Velocity measurements over smooth and L-groove surfaces 132 Figure 4.38 Velocity measurements over smooth and U-groove surfaces 133 Figure 4.39 Figure 4.40 Figure 4.41 Figure 4.42 Velocity measurements over smooth and riblets with groove height 600µm 134 Velocity measurements over smooth and riblets with groove height 800µm 134 Velocity measurements over smooth and riblets with groove height 1000µm 135 The RMS values of the velocity profiles of triangular, trapezoidal, spaced triangular, L-groove and U-groove of 600µm height dimension at Reynolds number 138 xiii

18 LIST OF SYMBOLS A Area Skin friction coefficient Wall shear stress ( Channel hydraulic diameter (mm) P Wetted perimeter of the duct L length of the test section (m) P Pressure (Pa) Pressure drop over smooth surface (Pa) Pressure drop over rib surface (Pa) Re Reynolds Number u Mean velocity ( Kinematic viscosity ( ) Density h Riblet height (µm) s Peak-to-peak riblet spacing (µm) Groove tip (µm) Groove base (µm) h + Non-dimensional groove height + Non-dimensional groove space Ɛ Turbulent energy dissipation rate per unit mass (m 2 /s 3 ) xiv

19 LIST OF ABBREVIATIONS DRA OLDs BLADEs LEBUs TAPPMs WEDM CNC LDV LIF Drag Reducing Agents Outer Layer Devices Boundary Layer Devices Large Eddy Breakup Devices Tandem Arrayed Parallel Plate Manipulator Wire Electrical discharge Machining Computer Numerical Controlled Milling Machine Laser Doppler Velocimetry Laser Induced Florescence xv