Biological flapping wing flyers achieve flight maneuverability and efficiency in low speed flight environments that has not been replicated by man-made flyers. Micro Air Vehicle (MAV) design goals are to develop flyers that maintain flight in environments that biological flyers excel in which includes low speeds, hovering, and urban settings. This flight is characterized by flow phenomena that are not well understood such as: flow separation and vortical flow. The goal of this study is to perform a literature review about the aerodynamics of flapping flight and discuss the application to MAV design. The study will evaluate the design initiatives of MAV. Experimental and computational test methods are reviewed. Low Reynolds number aerodynami...
The purpose of this research is to design and fabricate a flapping wing micro air vehicle (MAV) usin...
During the sampling of atmospheric aerosol particles from ambient environments, particles must be se...
Optimum wing spanloads were evaluated by comparing wing performance values from theoretical predicti...
Biological flapping wing flyers achieve flight maneuverability and efficiency in low speed flight en...
Flapping wings may have potential for success in the realm of micro air vehicles (MAVs). The goal of...
This thesis describes the concept, design and testing of a micro air vehicle rotor testbed capable o...
An analytical model of flapping membrane wing aerodynamics using experimental kinematic data is pres...
The objective of this research is to verify the three degree of freedom capabilities of a bio-inspir...
The goal of the present research is to understand aerodynamics at low Reynolds numbers and synthesiz...
The hovering flight of a micro air vehicle was investigated. Various flight control concepts, inspir...
The flight dynamics, stability, and control of a model flapping wing micro air vehicle are analyzed ...
The development and use of Micro Air Vehicles is becoming more and more important to the military. S...
Many creatures in nature have evolved the ability to fly and some seem to do so effortlessly with ca...
A wing-embedded Cross-Flow Fan (CFF) was first proposed as an active flow control (AFC) device nearl...
Micro air vehicles, or MAVs, are of current interest for a multitude of uses to which they, being sm...
The purpose of this research is to design and fabricate a flapping wing micro air vehicle (MAV) usin...
During the sampling of atmospheric aerosol particles from ambient environments, particles must be se...
Optimum wing spanloads were evaluated by comparing wing performance values from theoretical predicti...
Biological flapping wing flyers achieve flight maneuverability and efficiency in low speed flight en...
Flapping wings may have potential for success in the realm of micro air vehicles (MAVs). The goal of...
This thesis describes the concept, design and testing of a micro air vehicle rotor testbed capable o...
An analytical model of flapping membrane wing aerodynamics using experimental kinematic data is pres...
The objective of this research is to verify the three degree of freedom capabilities of a bio-inspir...
The goal of the present research is to understand aerodynamics at low Reynolds numbers and synthesiz...
The hovering flight of a micro air vehicle was investigated. Various flight control concepts, inspir...
The flight dynamics, stability, and control of a model flapping wing micro air vehicle are analyzed ...
The development and use of Micro Air Vehicles is becoming more and more important to the military. S...
Many creatures in nature have evolved the ability to fly and some seem to do so effortlessly with ca...
A wing-embedded Cross-Flow Fan (CFF) was first proposed as an active flow control (AFC) device nearl...
Micro air vehicles, or MAVs, are of current interest for a multitude of uses to which they, being sm...
The purpose of this research is to design and fabricate a flapping wing micro air vehicle (MAV) usin...
During the sampling of atmospheric aerosol particles from ambient environments, particles must be se...
Optimum wing spanloads were evaluated by comparing wing performance values from theoretical predicti...