The two-dimensional (2D) inclined stroke plane kinematics of insect wing is studied for various stroke plane angles using the Immersed Boundary (IB) solver. The numerical results revealed the dominant lift enhancement mechanisms for this class of flows. The generated dipole was analyzed to find the maximum velocity, inclination and spread. The analysis of these dipole characteristics for the different stroke plane angles exposed the alternate method to study the vertical force variation with the stroke plane angles. Lift enhancement mechanisms and dipole characteristics complement the high vertical force coefficient for the stroke plane angle of 60˚ commonly used by dragonflies during hover. The location of the dipole identified a region of...
The computational fluid dynamic model of a live-sized dragonfly (Sympetrum flaveolum) hindwing is si...
Thesis (Ph.D.)--University of Washington, 2017-03A dynamic model of an insect wing is developed trea...
The development of micro aerial vehicles is motivated by the need for autonomous unmanned aerial veh...
The two-dimensional (2D) inclined stroke plane kinematics of insect wing is studied for various stro...
Recent interest in developing micro air vehicles (MAVs) for a variety of both civil and military use...
Flapping flight has gained much attention in the past decade driven by the desire to understand capa...
In this study, mathematical modeling of fluid flow and numerical simulations were used to determine ...
The aerodynamic force and the flow structure of a wing performing hovering motion at small Reynolds ...
The development of Micro Aerial Vehicles (MAVs) has led researchers to study insects in order to bet...
International audienceFlight agility, resistance to gusts, capability to hover coupled with a low no...
An Unsteady force generation mechanisms (delayed stall, wake capture and rotational lift) during ide...
The motivation of the current study is to explore two major aspects of flapping flight in insects: t...
Numerical simulations are conducted to investigate of aerodynamic force generation for the figure-of...
Through two-dimensional numerical simulations, the fluid dynamic consequences of varying the Reynold...
Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.Includes...
The computational fluid dynamic model of a live-sized dragonfly (Sympetrum flaveolum) hindwing is si...
Thesis (Ph.D.)--University of Washington, 2017-03A dynamic model of an insect wing is developed trea...
The development of micro aerial vehicles is motivated by the need for autonomous unmanned aerial veh...
The two-dimensional (2D) inclined stroke plane kinematics of insect wing is studied for various stro...
Recent interest in developing micro air vehicles (MAVs) for a variety of both civil and military use...
Flapping flight has gained much attention in the past decade driven by the desire to understand capa...
In this study, mathematical modeling of fluid flow and numerical simulations were used to determine ...
The aerodynamic force and the flow structure of a wing performing hovering motion at small Reynolds ...
The development of Micro Aerial Vehicles (MAVs) has led researchers to study insects in order to bet...
International audienceFlight agility, resistance to gusts, capability to hover coupled with a low no...
An Unsteady force generation mechanisms (delayed stall, wake capture and rotational lift) during ide...
The motivation of the current study is to explore two major aspects of flapping flight in insects: t...
Numerical simulations are conducted to investigate of aerodynamic force generation for the figure-of...
Through two-dimensional numerical simulations, the fluid dynamic consequences of varying the Reynold...
Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.Includes...
The computational fluid dynamic model of a live-sized dragonfly (Sympetrum flaveolum) hindwing is si...
Thesis (Ph.D.)--University of Washington, 2017-03A dynamic model of an insect wing is developed trea...
The development of micro aerial vehicles is motivated by the need for autonomous unmanned aerial veh...