In this study, we evaluated the lift force generated by the crane-fly\u27s flapping wing with the passive pitching using the dynamically scaled model. Since the wing and the surrounding fluid interact with each other, the dynamic similarity between the model and actual crane-fly flights was measured using not only the Reynolds and Strouhal numbers but also the mass and Cauchy numbers. Although there existed the defference between the mass number due to the constant acceleration of the gravity, but the lift coefficient similated by our model indicated that the flapping wing with the passive pitching produces the enough lift force to supprt the crane-fly\u27s weight
Quasi-steady aerodynamic models play an important role in evaluating aerodynamic performance and con...
Abstract. In order to study the forces acting on a flapping wing, an experimental investigation is p...
Using a combination of force transducer measurement to quantify net lift force, high frame rate came...
In this study, we evaluated the lift force generated by the crane-fly's flapping wing with the passi...
A flapping flight mechanism of a Red-crowned crane (Grus japonensis) in migration was estimated usin...
Experiments were conducted to collect dynamic force measurements on a pitching wing using canonical ...
Graduation date: 2014There is a pressing need for Micro Air Vehicles (MAV) that are light, powerful,...
In the paper, a novel flapping mode is presented that can generate high lift force by a dragonfly wi...
This study successfully described the mechanics of flapping hovering flight within the framework of ...
Wing pitch reversal, the rapid change of angle of attack near stroke transition, repre-sents a diffe...
This thesis concerns the experimental analysis of the aerodynamics and aeroelasticity of oscillatin...
Effects of flexibility on the force generation and the propulsive efficiency of flapping flexible wi...
Dynamically stretching and retracting wingspan has been widely observed in the flight of birds and b...
This project consists in a parametric study of force generation in flapping wings. The first part i...
In this work, we use a three-dimensional computational fluid dynamics (CFD) simulation to comprehend...
Quasi-steady aerodynamic models play an important role in evaluating aerodynamic performance and con...
Abstract. In order to study the forces acting on a flapping wing, an experimental investigation is p...
Using a combination of force transducer measurement to quantify net lift force, high frame rate came...
In this study, we evaluated the lift force generated by the crane-fly's flapping wing with the passi...
A flapping flight mechanism of a Red-crowned crane (Grus japonensis) in migration was estimated usin...
Experiments were conducted to collect dynamic force measurements on a pitching wing using canonical ...
Graduation date: 2014There is a pressing need for Micro Air Vehicles (MAV) that are light, powerful,...
In the paper, a novel flapping mode is presented that can generate high lift force by a dragonfly wi...
This study successfully described the mechanics of flapping hovering flight within the framework of ...
Wing pitch reversal, the rapid change of angle of attack near stroke transition, repre-sents a diffe...
This thesis concerns the experimental analysis of the aerodynamics and aeroelasticity of oscillatin...
Effects of flexibility on the force generation and the propulsive efficiency of flapping flexible wi...
Dynamically stretching and retracting wingspan has been widely observed in the flight of birds and b...
This project consists in a parametric study of force generation in flapping wings. The first part i...
In this work, we use a three-dimensional computational fluid dynamics (CFD) simulation to comprehend...
Quasi-steady aerodynamic models play an important role in evaluating aerodynamic performance and con...
Abstract. In order to study the forces acting on a flapping wing, an experimental investigation is p...
Using a combination of force transducer measurement to quantify net lift force, high frame rate came...