Designing horizontal-axis wind turbine (HAWT) blades to achieve satisfactory levels of performance starts with knowledge of the aerodynamic forces acting on the blades. In this thesis, HAWT blade design is studied from the aspect of aerodynamic view and the basic principles of the aerodynamic behaviors of HAWTs are investigated. Blade-element momentum theory (BEM) known as also strip theory, which is the current mainstay of aerodynamic design and analysis of HAWT blades, is used for HAWT blade design in this thesis. Firstly, blade design procedure for an optimum rotor according to BEM theory is performed. Then designed blade shape is modified such that modified blade will be lightly loaded regarding the highly loaded of the designed blade and power prediction of modified blade is analyzed. When the designed blade shape is modified, it is seen that the power extracted from the wind is reduced about 10% and the length of modified blade is increased about 5% for the same required power. BLADESIGN which is a user-interface computer program for HAWT blade design is written. It gives blade geometry parameters (chord-length and twist distributions) and design conditions (design tip-speed ratio, design power coefficient and rotor diameter) for the following inputs / power required from a turbine, number of blades, design wind velocity and blade profile type (airfoil type). The program can be used by anyone who may not be intimately concerned with the concepts of blade design procedure and the results taken from the program can be used for further studies.

Small scale wind turbines operating in an urban environment produce dismal amounts of power when compared to their expected output [1-4]. This is largely due to the gusty wind conditions found in an urban environment, coupled with the fact that the wind turbines are not designed for these conditions. A new concept of a Segmented Variable Pitch (SVP) wind turbine has been proposed, which has a strong possibility to perform well in gusty and variable wind conditions. This dissertation explains the concept of a SVP wind turbine in more detail and shows analytical and experimental results relating to this concept. Also, the potential benefits of the proposed concept are mentioned. The results from this dissertation show that this concept has potential with promising results on possible turbine blade aerofoil configurations. Scaled model tests were completed and although further design optimisation is required, the tests showed good potential for the SVP concept. Lastly a proof-of-concept full scale model was manufactured and tested to prove scalability to full size from concept models. Along with the proof-of-concept full scale model, a wireless control system (to control the blade segments) was developed and tested.

The typical methodology for analytically designing a wind turbine blade is by means of blade element momentum (BEM) theory, whereby the aerofoil angle of attack is optimized to achieve a maximum lift-to-drag ratio. This research aims to show that an alternative optimisation methodology could yield better results, especially in gusty and turbulent wind conditions. This alternative method looks at increasing the aerofoil Reynolds number by increasing the aerofoil chord length. The increased Reynolds number generally increases the e_ectiveness of the aerofoil which would result in a higher or similar lift-to-drag ratio (even at the decreased angle of attacked require to maintain the turbine thrust coe_cient). The bene_t of this design is a atter power curve which causes the turbine to be less sensitive to uctuating winds. Also, the turbine has more torque at startup, allowing for operatation in lower wind speeds. This research is assumed to only be applicable to small wind turbines which operated in a low Reynolds number regime (<500 000), where Reynolds number manipulation is most advantageous.

Background: Historically, many reference lines and planes of the human skull have been used in an attempt to depict the head in a natural head position (NHP) which is a relaxed/balanced position when looking ahead at their eye level. Head position correction has been attempted in fields such as anatomy, art, anthropology, orthodontics, oral and maxillofacial surgery, plastic surgery, and forensics. In orthodontics, oral and maxillofacial surgery, and plastic surgery, corrected head position (CHP) is particularly important for diagnosis of the normality/protrusion/retrusion of the patient’s facial skeleton. Usually a single plane, such as Frankfurt horizontal, is used to correct head position, but its angulation is variable between individuals, because each individual’s anatomy is unique. It has been found previously that the Neutral Horizontal Axis (NHA), Frankfurt horizontal (FH), Krogman-Walker plane (KW plane), and Palatal plane (P plane) demonstrated near parallelism, and these planes averaged -1 to -2 degrees from the true horizontal (HOR, which is a horizontal plane determined as being perpendicular to the earth’s gravitational force) with subjects in NHP. Methods: Craniofacial planes were measured in an Aboriginal Australian sample and in two contemporary samples obtained from Australian orthodontic practices, and the findings were compared with previous studies. Each sample consisted of 40 individuals (20 males and 20 females) with subjects in NHP. The Aboriginal Australian sample was longitudinal (T1, mean age 10 years; T2, mean age 14 years, and T3, mean age 18 years) enabling NHP to be assessed over approximately 8 years. A soft tissue Ear - nose plane (EN plane) was also investigated. Results: NHP reproducibility over 8 years demonstrated a mean of absolute difference of 2.9 degrees, with a range of differences from -7.9 to 8.2 degrees and a standard deviation of differences equal to 3.6 degrees. The Neutral Horizontal Axis (NHA), Frankfurt horizontal (FH), Krogman-Walker plane (KW plane), and Palatal plane (P plane) demonstrated near parallelism with each other, and averaged between 0 and -3 degrees from HOR. On average, EN plane was horizontal but was variable. Conclusions: NHP is not consistently reproducible at the individual level. For hard tissue images, the combined use of NHA, FH, KW plane, and P plane enables prediction of CHP. Additionally, the rectangular shape of the lower orbit - nasal airway region appears to be useful for correcting head position. In facial soft tissue images, EN plane in combination with other visual factors helps to correct head position. Simple geometry enables this head position correction to be performed from any view of the head where relevant landmarks are seen. / http://proxy.library.adelaide.edu.au/login?url= http://library.adelaide.edu.au/cgi-bin/Pwebrecon.cgi?BBID=1346599 / Thesis (D.Clin.Dent.) - University of Adelaide, School of Dentistry, 2008

Background: Historically, many reference lines and planes of the human skull have been used in an attempt to depict the head in a natural head position (NHP) which is a relaxed/balanced position when looking ahead at their eye level. Head position correction has been attempted in fields such as anatomy, art, anthropology, orthodontics, oral and maxillofacial surgery, plastic surgery, and forensics. In orthodontics, oral and maxillofacial surgery, and plastic surgery, corrected head position (CHP) is particularly important for diagnosis of the normality/protrusion/retrusion of the patient’s facial skeleton. Usually a single plane, such as Frankfurt horizontal, is used to correct head position, but its angulation is variable between individuals, because each individual’s anatomy is unique. It has been found previously that the Neutral Horizontal Axis (NHA), Frankfurt horizontal (FH), Krogman-Walker plane (KW plane), and Palatal plane (P plane) demonstrated near parallelism, and these planes averaged -1 to -2 degrees from the true horizontal (HOR, which is a horizontal plane determined as being perpendicular to the earth’s gravitational force) with subjects in NHP. Methods: Craniofacial planes were measured in an Aboriginal Australian sample and in two contemporary samples obtained from Australian orthodontic practices, and the findings were compared with previous studies. Each sample consisted of 40 individuals (20 males and 20 females) with subjects in NHP. The Aboriginal Australian sample was longitudinal (T1, mean age 10 years; T2, mean age 14 years, and T3, mean age 18 years) enabling NHP to be assessed over approximately 8 years. A soft tissue Ear - nose plane (EN plane) was also investigated. Results: NHP reproducibility over 8 years demonstrated a mean of absolute difference of 2.9 degrees, with a range of differences from -7.9 to 8.2 degrees and a standard deviation of differences equal to 3.6 degrees. The Neutral Horizontal Axis (NHA), Frankfurt horizontal (FH), Krogman-Walker plane (KW plane), and Palatal plane (P plane) demonstrated near parallelism with each other, and averaged between 0 and -3 degrees from HOR. On average, EN plane was horizontal but was variable. Conclusions: NHP is not consistently reproducible at the individual level. For hard tissue images, the combined use of NHA, FH, KW plane, and P plane enables prediction of CHP. Additionally, the rectangular shape of the lower orbit - nasal airway region appears to be useful for correcting head position. In facial soft tissue images, EN plane in combination with other visual factors helps to correct head position. Simple geometry enables this head position correction to be performed from any view of the head where relevant landmarks are seen. / http://proxy.library.adelaide.edu.au/login?url= http://library.adelaide.edu.au/cgi-bin/Pwebrecon.cgi?BBID=1346599 / Thesis (D.Clin.Dent.) - University of Adelaide, School of Dentistry, 2008

A evolução do uso da energia eólica nas últimas décadas está diretamente relacionada ao desenvolvimento da tecnologia empregada na conversão e projeto das instalações. A viabilização de uma instalação eólica de grande porte depende da avaliação correta do potencial eólico. A fim de avaliar a capacidade de conversão de energia cinética do vento em torque, é fundamental a modelagem da esteira aerodinâmica das turbinas eólicas. Este trabalho apresenta um estudo sobre a esteira aerodinâmica formada por uma turbina eólica dimensionada conforme a teoria de otimização de Betz. Para tanto, realiza-se inicialmente uma pesquisa sobre a evolução da transformação da energia contida no vento em energia mecânica e métodos de análise adotados. Para modelagem da esteira, realiza-se a simulação numérica do escoamento sobre uma turbina de eixo horizontal empregando o Método de Volumes Finitos. Através do uso da Dinâmica dos Fluidos Computacional são resolvidas as Equações de Navier-Stokes com Médias de Reynolds (RANS) e a utilização dos modelos de turbulência k-, k- RNG, k- e k- SST. Para a solução das equações é utilizado o programa ANSYS-CFX. Define-se o perfil NACA 4412 como perfil aerodinâmico para projeto das pás da turbina, e modela-se a turbina através da teoria de dimensionamento ótimo de Betz. O domínio, discretizado em um número finito de volumes de controle, possui duas regiões distintas, uma estática e outra rotacional, representado o rotor da turbina. Inicialmente são apresentadas simulações com os diferentes modelos de turbulência e definido o modelo que apresenta os melhores resultados, o k- SST. Para o modelo escolhido são realizadas simulações incluindo estudos com a turbina inclinada em relação à direção de incidência do vento, para verificar a alteração no perfil da esteira gerada e na capacidade da turbina em transformar a energia do vento em Torque. Os resultados obtidos para os campos de velocidade e pressão são comparados com os de outros autores e mostraram-se coerentes, indicando que a simulação feita é capaz de representar o fenômeno analisado. / The evolution of the use of the wind energy in recent decades is directly related to the technology in the facilities conversion and design. The feasibility of a large wind farm depends on the correct assessment of wind potential. To evaluate the capacity of converting wind kinetic energy in torque, it is essential to model the wake aerodynamics of wind turbines. This paper presents a study on the aerodynamic wake formed by a wind turbine sized according to the Betz optimization theory. For this, initially it is performed a research on the evolution of the energy contained in wind into mechanical energy and the adopted analysis methods. For wake modeling, a horizontal axis wind turbine flow numerical simulation is done using the Finite Volume Method. Using the Computational Fluid Dynamics, the Reynolds Averaged Navier-Stokes equations are solved with the use of the k-, k- RNG, k- e k- SST turbulence models and using the software ANSYS-CFX. It is defined the NACA 4412 profile as aerodynamic profile for turbine blades and the turbine is modeled using the Betz optimization theory. The domain, discretized into a finite number of control volumes, has two distinct regions, one static and one rotational, represented the turbine rotor. Initially the simulations with different turbulence models are presented and the model k- SST is defined as the model that gives best results. For the chosen model, simulations are performed, including studies on the turbine yawed with respect to the wind incidence direction, to verify the profile change in the generated wake and turbine capacity to convert wind energy into torque. The obtained results for the velocity and pressure fields are compared to other authors are very consistent, indicating that the proposed simulation is capable of representing the analyzed phenomenon.

A evolução do uso da energia eólica nas últimas décadas está diretamente relacionada ao desenvolvimento da tecnologia empregada na conversão e projeto das instalações. A viabilização de uma instalação eólica de grande porte depende da avaliação correta do potencial eólico. A fim de avaliar a capacidade de conversão de energia cinética do vento em torque, é fundamental a modelagem da esteira aerodinâmica das turbinas eólicas. Este trabalho apresenta um estudo sobre a esteira aerodinâmica formada por uma turbina eólica dimensionada conforme a teoria de otimização de Betz. Para tanto, realiza-se inicialmente uma pesquisa sobre a evolução da transformação da energia contida no vento em energia mecânica e métodos de análise adotados. Para modelagem da esteira, realiza-se a simulação numérica do escoamento sobre uma turbina de eixo horizontal empregando o Método de Volumes Finitos. Através do uso da Dinâmica dos Fluidos Computacional são resolvidas as Equações de Navier-Stokes com Médias de Reynolds (RANS) e a utilização dos modelos de turbulência k-, k- RNG, k- e k- SST. Para a solução das equações é utilizado o programa ANSYS-CFX. Define-se o perfil NACA 4412 como perfil aerodinâmico para projeto das pás da turbina, e modela-se a turbina através da teoria de dimensionamento ótimo de Betz. O domínio, discretizado em um número finito de volumes de controle, possui duas regiões distintas, uma estática e outra rotacional, representado o rotor da turbina. Inicialmente são apresentadas simulações com os diferentes modelos de turbulência e definido o modelo que apresenta os melhores resultados, o k- SST. Para o modelo escolhido são realizadas simulações incluindo estudos com a turbina inclinada em relação à direção de incidência do vento, para verificar a alteração no perfil da esteira gerada e na capacidade da turbina em transformar a energia do vento em Torque. Os resultados obtidos para os campos de velocidade e pressão são comparados com os de outros autores e mostraram-se coerentes, indicando que a simulação feita é capaz de representar o fenômeno analisado. / The evolution of the use of the wind energy in recent decades is directly related to the technology in the facilities conversion and design. The feasibility of a large wind farm depends on the correct assessment of wind potential. To evaluate the capacity of converting wind kinetic energy in torque, it is essential to model the wake aerodynamics of wind turbines. This paper presents a study on the aerodynamic wake formed by a wind turbine sized according to the Betz optimization theory. For this, initially it is performed a research on the evolution of the energy contained in wind into mechanical energy and the adopted analysis methods. For wake modeling, a horizontal axis wind turbine flow numerical simulation is done using the Finite Volume Method. Using the Computational Fluid Dynamics, the Reynolds Averaged Navier-Stokes equations are solved with the use of the k-, k- RNG, k- e k- SST turbulence models and using the software ANSYS-CFX. It is defined the NACA 4412 profile as aerodynamic profile for turbine blades and the turbine is modeled using the Betz optimization theory. The domain, discretized into a finite number of control volumes, has two distinct regions, one static and one rotational, represented the turbine rotor. Initially the simulations with different turbulence models are presented and the model k- SST is defined as the model that gives best results. For the chosen model, simulations are performed, including studies on the turbine yawed with respect to the wind incidence direction, to verify the profile change in the generated wake and turbine capacity to convert wind energy into torque. The obtained results for the velocity and pressure fields are compared to other authors are very consistent, indicating that the proposed simulation is capable of representing the analyzed phenomenon.

Thesis submitted in fulfilment of the requirements for the degree MAGISTER TECHNOLOGIAE: Mechanical Engineering in the FACULTY OF ENGINEERING at the CAPE PENINSULA UNIVERSITY OF TECHNOLOGY, 2012 / The amount of power a horizontal axis wind turbine (HAWT) can produce is determined by two main factors, wind velocity and rotor swept area. Theory dictates that the power production of a horizontal wind turbine is related to the cube of wind velocity and the square of the turbine diameter (or radius). The power produced at any given time is thus dependent on of the wind velocity and the rotor swept area of the turbine. Wind is variable in availability and consistency. Very little can be done to effect the wind velocity passing through the turbine rotor area and its effect is minimal. Thus understandably if more power is required, from the same wind velocity, the rotor diameter must be increased. A variable length blade can adapt lengthwise to accommodate low wind velocities and similarly high wind velocities during extreme conditions, thus increasing the operational time and power production of the turbine. The work undertaken in this thesis is a comparative study between standard design, fixed length blades to that of a modified design, variable length blade. The project entailed the design and development of small diameter HAWT blades and experimental testing. The turbine blades were designed using applicable theory and manufactured from available materials. For the experiments, the turbine was mounted on a vehicle and driven at various speeds. Due to size limitations, no dynamic adaption was done during testing. The variable length design blade was obtained by cutting increments off. The results obtained from each test were compared at corresponding points and conditions. Final interpretation of results lead to the conclusion that by increasing or decreasing the turbine blade length the area of turbine energy capture can be adjusted to affect the amount of power produced. Additional benefits included, force reduction during extreme operating conditions, extended production period for the turbine and a mechanical start up method during low wind speeds. The financial feasibility did not form part of the scope of this thesis and the technical feasibility of the concept can be thoroughly addressed in future research.

A evolução do uso da energia eólica nas últimas décadas está diretamente relacionada ao desenvolvimento da tecnologia empregada na conversão e projeto das instalações. A viabilização de uma instalação eólica de grande porte depende da avaliação correta do potencial eólico. A fim de avaliar a capacidade de conversão de energia cinética do vento em torque, é fundamental a modelagem da esteira aerodinâmica das turbinas eólicas. Este trabalho apresenta um estudo sobre a esteira aerodinâmica formada por uma turbina eólica dimensionada conforme a teoria de otimização de Betz. Para tanto, realiza-se inicialmente uma pesquisa sobre a evolução da transformação da energia contida no vento em energia mecânica e métodos de análise adotados. Para modelagem da esteira, realiza-se a simulação numérica do escoamento sobre uma turbina de eixo horizontal empregando o Método de Volumes Finitos. Através do uso da Dinâmica dos Fluidos Computacional são resolvidas as Equações de Navier-Stokes com Médias de Reynolds (RANS) e a utilização dos modelos de turbulência k-, k- RNG, k- e k- SST. Para a solução das equações é utilizado o programa ANSYS-CFX. Define-se o perfil NACA 4412 como perfil aerodinâmico para projeto das pás da turbina, e modela-se a turbina através da teoria de dimensionamento ótimo de Betz. O domínio, discretizado em um número finito de volumes de controle, possui duas regiões distintas, uma estática e outra rotacional, representado o rotor da turbina. Inicialmente são apresentadas simulações com os diferentes modelos de turbulência e definido o modelo que apresenta os melhores resultados, o k- SST. Para o modelo escolhido são realizadas simulações incluindo estudos com a turbina inclinada em relação à direção de incidência do vento, para verificar a alteração no perfil da esteira gerada e na capacidade da turbina em transformar a energia do vento em Torque. Os resultados obtidos para os campos de velocidade e pressão são comparados com os de outros autores e mostraram-se coerentes, indicando que a simulação feita é capaz de representar o fenômeno analisado. / The evolution of the use of the wind energy in recent decades is directly related to the technology in the facilities conversion and design. The feasibility of a large wind farm depends on the correct assessment of wind potential. To evaluate the capacity of converting wind kinetic energy in torque, it is essential to model the wake aerodynamics of wind turbines. This paper presents a study on the aerodynamic wake formed by a wind turbine sized according to the Betz optimization theory. For this, initially it is performed a research on the evolution of the energy contained in wind into mechanical energy and the adopted analysis methods. For wake modeling, a horizontal axis wind turbine flow numerical simulation is done using the Finite Volume Method. Using the Computational Fluid Dynamics, the Reynolds Averaged Navier-Stokes equations are solved with the use of the k-, k- RNG, k- e k- SST turbulence models and using the software ANSYS-CFX. It is defined the NACA 4412 profile as aerodynamic profile for turbine blades and the turbine is modeled using the Betz optimization theory. The domain, discretized into a finite number of control volumes, has two distinct regions, one static and one rotational, represented the turbine rotor. Initially the simulations with different turbulence models are presented and the model k- SST is defined as the model that gives best results. For the chosen model, simulations are performed, including studies on the turbine yawed with respect to the wind incidence direction, to verify the profile change in the generated wake and turbine capacity to convert wind energy into torque. The obtained results for the velocity and pressure fields are compared to other authors are very consistent, indicating that the proposed simulation is capable of representing the analyzed phenomenon.

Small wind turbines that operate in low-wind environments are prone to suffer performance degradation as they often fail to accelerate to a steady, power-producing condition. The behaviour during this process is called “starting behaviour” and it is the subject of this present work. This thesis evaluates potential benefits that can be obtained from the improvement of starting behaviour, investigates, in particular, small wind turbine starting behaviour (both horizontal- and vertical-axis), and presents aerofoil performance characteristics (both steady and unsteady) needed for the analysis. All of the investigations were conducted using a new set of aerodynamic performance data of six aerofoils (NACA0012, SG6043, SD7062, DU06-W-200, S1223, and S1223B). All of the data were obtained at flow conditions that small wind turbine blades have to operate with during the startup - low Reynolds number (from 65000 to 150000), high angle of attack (through 360◦), and high reduced frequency (from 0.05 to 0.20). In order to obtain accurate aerodynamic data at high incidences, a series of CFD simulations were undertaken to illustrate effects of wall proximity and to determine test section sizes that offer minimum proximity effects. A study was carried out on the entire horizontal-axis wind turbine generation system to understand its starting characteristics and to estimate potential benefits of improved starting. Comparisons of three different blade configurations reveal that the use of mixed-aerofoil blades leads to a significant increase in starting capability. The improved starting capability effectively reduces the time that the turbine takes to reach its power-extraction period and, hence, an increase in overall energy yield. The increase can be as high as 40%. Investigations into H-Darriues turbine self-starting capability were made through the analogy between the aerofoil in Darrieus motion and flapping-wing flow mechanisms. The investigations reveal that the unsteadiness associated with the rotor is key to predicting its starting behaviour and the accurate prediction can be made when this transient aerofoil behaviour is correctly modelled. The investigations based upon the analogy also indicate that the unsteadiness can be exploited to promote the turbine ability to self-start. Aerodynamically, this exploitation is related to the rotor geometry itself.