Fluid Mechanics in Channel, Pipe and Aerodynamic Design Geometries 2

Name: Fluid Mechanics in Channel, Pipe and Aerodynamic Design Geometries 2
Brand: Wiley-Scrivener
Price: 139.99 EUR
Availability: OnlineOnly

Christina G. Georgantopoulou George A. Georgantopoulos(Autor*in)

Wiley-Scrivener (Verlag)

1. Auflage

Erschienen am 16. April 2018

304 Seiten

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978-1-119-52238-6 (ISBN)

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Inhalt

Cover
Half-Title Page
Dedication
Title Page
Copyright Page
Contents
Preface
1. Pipe Networks
1.1. Introduction
1.2. Calculation of pipe networks
1.3. Problem-solving methodology for pipe networks
1.4. Overall approach for the network calculation
1.5. The Hazen-Williams equation for network analysis
1.6. Hazen-Williams and Darcy-Weisbach identity
1.7. Hardy-Cross method
1.8. Formulae
1.9. Questions
1.10. Problems with solutions
1.11. Problems to be solved
2. Open Channel Flow
2.1. Introduction
2.2. Non-dimensional parameters in open channels
2.3. Open channel types of flow
2.4. Open channels' geometrical shapes
2.4.1. Channels of rectangular cross-sectional area
2.4.2. Channels of trapezoidal cross-sectional area
2.4.3. Channels of circular cross-sectional area
2.5. The hydraulic jump
2.6. Calculation of the depth flow after the hydraulic jump
2.7. Velocity distribution
2.8. Velocity distribution at the vertical level
2.9. Uniform flow in open channel equations - Chezy type
2.10. Best hydraulic cross-sectional area
2.11. Specific flow energy
2.12. Channels of rectangular cross-sectional area
2.13. Open channels' more adequate cross-sectional areas
2.13.1. Rectangular cross-sectional area
2.13.2. Trapezoidal cross-sectional area
2.14. Non-uniform flow in open channels
2.15. Channels of non-rectangular cross-section area
2.16. Formulae
2.16.1. Channels of rectangular cross-sectional area formulae
2.16.2. Channels of trapezoidal cross-section formulae
2.16.3. Channels of circular cross-sectional area formulae
2.16.4. Channels of rectangular cross-sectional area formulae
2.16.5. Channels of non-rectangular cross-sectional area formulae
2.17. Questions
2.18. Problems with solutions
2.19. Problems to be solved
3. Boundary Layer
3.1. Introduction
3.2. Laminar incompressible boundary layer
3.3. Characteristic values of the boundary layer
3.3.1. Thickness d of the boundary layer
3.3.2. The thickness displacement d´1
3.4. Flow types in the boundary layer
3.5. Formulae
3.6. Questions
3.7. Problems with solutions
3.8. Problems to be solved
4. Flow Around Solid Bodies
4.1. Introduction
4.2. Geometrical characteristics of an airfoil
4.3. Kutta-Joukowski equation
4.4. Aerodynamic paradox
4.5. Pressure distribution in an airfoil
4.6. Lift curve
4.7. Drag force and drag coefficient curve
4.7.1. Drag of skin friction
4.7.2. Form drag
4.7.3. Induced drag
4.8. Parameters that influence the drag coefficient
4.8.1. Dependence of CD on the body's shape
4.8.2. Dependence of CD on relative roughness
4.8.3. Dependence of CD on the Reynolds number
4.9. External flow around industrial solid bodies
4.9.1. Car's motion
4.9.2. Surface vessel's motion
4.9.3. Wind flow in ground constructions
4.9.4. Airplane's motion
4.10. Drag in fluid drops and gas bubbles in creeping flow
4.11. Formulae
4.12. Questions
4.13. Problems with solutions
4.14. Problems to be solved
Appendices
Appendix 1: Symbols and Units
Appendix 2: Tables and Diagrams of Natural Values
Appendix 3: Symbols and Basic Conversion Factors
Appendix 4: International Standard Atmosphere, SI Units
Appendix 5: International Standard Atmosphere, in BS
Appendix 6: NACA Airfoils' Diagrams
Bibliography
Index
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