The Fluid Dynamic Basis for Actuator Disc and Rotor Theories

Name: The Fluid Dynamic Basis for Actuator Disc and Rotor Theories
Brand: IOS Press,US
Price: 47.99 EUR
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Gijs van Kuik(Herausgeber*in)

IOS Press,US

1. Auflage

Erschienen am 15. Juni 2018

148 Seiten

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978-1-61499-866-2 (ISBN)

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Beschreibung

The first rotor performance predictions were published by Joukowsky exactly 100 years ago. Although a century of research has expanded the knowledge of rotor aerodynamics enormously, and modern computer power and measurement techniques now enable detailed analyses that were previously out of reach, the concepts proposed by Froude, Betz, Joukowsky and Glauert for modelling a rotor in performance calculations are still in use today, albeit with modifications and expansions.
This book is the result of the author's curiosity as to whether a return to these models with a combination of mathematics, dedicated computations and wind tunnel experiments could yield more physical insight and answer some of the old questions still waiting to be resolved. Although most of the work included here has been published previously, the book connects the various topics, linking them in a coherent storyline.
This book will be of interest to those working in all branches of rotor aerodynamics - wind turbines, propellers, ship screws and helicopter rotors. It has been written for proficient students and researchers, and reading it will demand a good knowledge of inviscid (fluid) mechanics.

Jens Norkaer Sorensen, DTU, Technical University of Denmark: "(...) a great piece of work, which in a consistent way highlights many of the items that the author has worked on through the years. All in all, an impressive contribution to the classical work on propellers/wind turbines."

Peter Schaffarczyk, Kiel University of Applied Sciences, Germany: "(...) a really impressive piece of work!"

Carlos Simao Ferreira, Technical University Delft: "This is a timely book for a new generation of rotor aerodynamicists from wind turbines to drones and personal air-vehicles. In a time where fast numerical solutions for aerodynamic design are increasingly available, a clear theoretical and fundamental formulation of the rotor-wake problem will help professionals to evaluate the validity of their design problem. 'The Fluid Dynamic Basis for Actuator Disc and Rotor Theories' is a pleasure to read, while the structure, text and figures are just as elegant as the theory presented."

The cover shows 'The Red Mill', by Piet Mondriaan, 1911, collection Gemeentemuseum Den Haag. Cover image: (c) 2018 Mondrian/Holtzman Trust.

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Inhalt

Intro
Title Page
Contents
Preface
Reading guide
Acknowledgements
Nomenclature
1. More than a century of rotor research
1.1. Introduction
1.2. History of the actuator disc momentum theory
1.2.1. The British School
1.2.2. The German and Russian School
1.2.3. The contribution of Joukowsky and Betz to the vortex theory of propellers
1.2.4. The Betz-Joukowsky limit for wind turbines
1.3. From actuator disc to rotor aerodynamics
1.4. Why this book?
2. Force fields in fluid dynamics
2.1. Introduction
2.2. The equation of motion and the coordinate systems
2.3. Equivalence of the kinematic and dynamic methods
2.4. Conservative and non-conservative force fields
2.5. Force fields and energy
2.5.1. Work done by force fields
2.5.2. Choice of reference system
2.5.3. Pressure as a conservative force in momentum balances
2.5.4. Pressure interpreted as potential energy
2.6. Definition of (non-)conservative forces as used in this book
2.7. Evaluation
3. Force fields and vorticity
3.1. Introduction
3.2. The role of Helmholtz's conservation laws
3.3. Generation of actuator disc vorticity
3.4. Convection of actuator disc vorticity
3.5. Convection of rotor vorticity
3.6. Evaluation
4. The disc as representation of a rotor
4.1. Introduction
4.2. Loads and power of a Joukowsky disc and rotor
4.2.1. The actuator disc equation
4.2.2. The rotor blade
4.2.3. Power and thrust coefficients for Joukowsky discs / rotors
4.3. The transition from a B-bladed rotor to the Joukowsky disc
4.4. Comparison of the flow fields of a disc and rotor
4.5. Evaluation
5. Analysis of Froude's actuator disc flows
5.1. Introduction
5.2. One-dimensional momentum theory
5.2.1. The momentum balance
5.2.2. Momentum theory without conservative forces
5.2.3. Momentum theory including conservative forces
5.2.4. Momentum theory applied per stream annulus
5.3. Numerical assessment of Froude's actuator disc performance
5.3.1. The model and accuracy of computation
5.3.2. Comparison of calculated performance with momentum theory results
5.3.3. Comparison with experimental results
5.4. Flow details
5.4.1. Flow and pressure patterns
5.4.2. Properties of the wake boundary
5.4.3. Pressure and velocity distribution at the disc
5.4.4. Pressure at the axis
5.4.5. Momentum balance per annulus
5.5. An engineering model for the velocity at a wind turbine disc
5.6. Evaluation
6. Analysis of Joukowsky's actuator disc flows
6.1. Introduction
6.2. Two dimensional momentum theory
6.2.1. The equations for a Joukowsky disc
6.2.2. The disc load
6.2.3. The far wake outside the vortex core
6.2.4. The vortex core
6.2.5. The momentum, mass and energy balance
6.3. Limit values of the Joukowsky momentum theory
6.3.1. Results for , 0.
6.3.2. Propeller discs with a wake of constant radius and with wake expansion
6.3.3. The static disc or disc in hover
6.3.4. The maximum efficiency of a wind turbine disc
6.3.5. The efficiency of propeller discs
6.4. Numerical assessment of flow details
6.4.1. The numerical model
6.4.2. Comparison of wind turbine and propeller discs at =1
6.4.3. Comparison of a wind turbine and propeller disc with similar wake expansion
6.4.4. The velocity at the disc
6.4.5. Momentum balance per annulus
6.5. The role of swirl
6.6. Comparison of the Joukowsky and Betz-Goldstein solutions
6.7. Evaluation
7. Special topics: Conservative loads at a thick disc and blade tip
7.1. Introduction
7.2. The generation of a Rankine vortex
7.2.1. Wu's actuator disc equation
7.2.2. The force field required to generate a Rankine vortex
7.2.3. Interpretation of the radial component of the load
7.2.4. Numerical assessment of the impact of the radial load
7.3. The rotor blade
7.3.1. Inboard motion of a tip vortex
7.3.2. Side step: conservative, spanwise load on an elliptic wing
7.3.3. Conservative and non-conservative blade loads
7.3.4. Experimental and numerical results for a model wind turbine rotor
7.3.5. Determination of the conservative tip load
7.3.6. The tip vortex trajectory
7.4. The role of conservative forces
7.5. Evaluation
8. From disc theory to BEM models: the tip correction
8.1. Introduction
8.2. Development of the tip correction
8.2.1. In BEM methods
8.2.2. In actuator disc, actuator line and lifting line methods
8.3. The distribution of the axial velocity
8.3.1. The radial distribution
8.3.2. The azimuthal distribution: averaged or at blade position
8.3.3. The azimuthal distribution: decambering of aerofoils
8.4. The radial distribution of blade
8.4.1. The aspect ratio as a measure for tip effects
8.4.2. Chordwise vorticity and conservative loads at the tip
8.5. Evaluation
9. Epilogue
Appendix A. Vector expressions in cylindrical coordinates
Appendix B. Balance of angular momentum
Appendix C. The blade load expressed as pressure distribution
Appendix D. The potential flow model
D.1. Components of the model
D.2. Convergence scheme
D.3. Verification, sensitivity and accuracy
Bibliography
Index

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