Microtabs (MT) consist of a small tab placed on the airfoil surface close to the trailing edge and perpendicular to the surface. A study to find the optimal position to improve airfoil aerodynamic performance is presented. Therefore, a parametric study of a MT mounted on the pressure surface of an airfoil has been carried out. The aim of the current study is to find the optimal MT size and location to increase airfoil aerodynamic performance and to investigate its influence on the power output of a 5 MW wind turbine. Firstly, a computational study of a MT mounted on the pressure surface of the airfoil DU91W(2)250 has been carried out and the best case has been found according to the largest lift-to-drag ratio. This airfoil has been selected...
Due to the growing need of sustainable energy technologies, wind energy is gaining more popularity d...
Wind turbines are large complex dynamically flexible structures that must operate un-der very turbul...
A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid...
Microtabs (MT) consist of a small tab placed on the airfoil surface close to the trailing edge and p...
The use of deployable microtabs on wind turbine blades has been proposed for the purpose of active l...
This study presents an innovative design of a microtab system for aerodynamic load control on horizo...
The cost of wind-generated electricity can be reduced by mitigating fatigue loads acting on the roto...
Increases in wind turbine size have made controlling loads on the blades an important consideration ...
[[abstract]]This research experimentally investigates the rotor aerodynamics of horizontal-axis, mic...
Finite micro-tabs have been investigated experimentally to evaluate the potential for load control o...
Microtabs (MTs) are a regularly used flow control device in terms of wind turbine optimization. The ...
Gurney flaps (GFs) and microtabs (MTs) are two of the most frequently used passive flow control devi...
Small wind turbine power generation systems have the potential to meet the electricity demand of the...
This project aims to study the performance of the Rutland 504 micro wind turbine by means of a numer...
Gurney flaps (GFs) and microtabs (MTs) are two of the most frequently used passive flow control devi...
Due to the growing need of sustainable energy technologies, wind energy is gaining more popularity d...
Wind turbines are large complex dynamically flexible structures that must operate un-der very turbul...
A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid...
Microtabs (MT) consist of a small tab placed on the airfoil surface close to the trailing edge and p...
The use of deployable microtabs on wind turbine blades has been proposed for the purpose of active l...
This study presents an innovative design of a microtab system for aerodynamic load control on horizo...
The cost of wind-generated electricity can be reduced by mitigating fatigue loads acting on the roto...
Increases in wind turbine size have made controlling loads on the blades an important consideration ...
[[abstract]]This research experimentally investigates the rotor aerodynamics of horizontal-axis, mic...
Finite micro-tabs have been investigated experimentally to evaluate the potential for load control o...
Microtabs (MTs) are a regularly used flow control device in terms of wind turbine optimization. The ...
Gurney flaps (GFs) and microtabs (MTs) are two of the most frequently used passive flow control devi...
Small wind turbine power generation systems have the potential to meet the electricity demand of the...
This project aims to study the performance of the Rutland 504 micro wind turbine by means of a numer...
Gurney flaps (GFs) and microtabs (MTs) are two of the most frequently used passive flow control devi...
Due to the growing need of sustainable energy technologies, wind energy is gaining more popularity d...
Wind turbines are large complex dynamically flexible structures that must operate un-der very turbul...
A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid...