Add to ORKGThe project presents the development of a computational integrated model of the flight of a MAV. The created tool is validated and tested for fixed and flapping wing configurations. This preliminary design integrates the computation of the aerodynamic forces of unsteady flow of flapping wings and the dynamic behaviour dependent on those forces. Linear and non-linear aerodynamic estimations are used. The dynamic model is completely originated in the project, as the integration of both parts.Ingeniería Aeroespacia
AbstractTo evaluate the propulsion system capabilities of a Flapping Micro Air Vehicle (FMAV), a new...
This paper discusses a methodology of analyzing the flight dynamic stability of a flapping wing Micr...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...
The project presents the development of a computational integrated model of the flight of a MAV. Th...
The project presents the development of a computational integrated model of the flight of a MAV. Th...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...
for several years. Based on the developed flapping-wing MAVs we study its dynamics and compare our r...
[[abstract]]The dynamics of a flapping-wing micro aerial vehicle (MAV) is studied in this paper. The...
The low Reynolds number aerodynamics of the flapping wing Micro-Air Vehicle (MAV) developed at NPS ...
The interest in Micro Air Vehicles (MAVs) has stimulated continuous research activities, in view of ...
A range of quasi-steady and unsteady aerodynamic models are used to predict the aerodynamic forces e...
The interest in Micro Air Vehicles (MAVs) has stimulated continuous research activities, in view of ...
@Cranfield University 2004. All rights reserved. No part of this publication may be reproduced witho...
Title from PDF of title page (University of Missouri--Columbia, viewed on June 6, 2012).The entire t...
This thesis is on computational fluid-structure interaction (FSI) modeling of bioinspired flapping-w...
AbstractTo evaluate the propulsion system capabilities of a Flapping Micro Air Vehicle (FMAV), a new...
This paper discusses a methodology of analyzing the flight dynamic stability of a flapping wing Micr...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...
The project presents the development of a computational integrated model of the flight of a MAV. Th...
The project presents the development of a computational integrated model of the flight of a MAV. Th...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...
for several years. Based on the developed flapping-wing MAVs we study its dynamics and compare our r...
[[abstract]]The dynamics of a flapping-wing micro aerial vehicle (MAV) is studied in this paper. The...
The low Reynolds number aerodynamics of the flapping wing Micro-Air Vehicle (MAV) developed at NPS ...
The interest in Micro Air Vehicles (MAVs) has stimulated continuous research activities, in view of ...
A range of quasi-steady and unsteady aerodynamic models are used to predict the aerodynamic forces e...
The interest in Micro Air Vehicles (MAVs) has stimulated continuous research activities, in view of ...
@Cranfield University 2004. All rights reserved. No part of this publication may be reproduced witho...
Title from PDF of title page (University of Missouri--Columbia, viewed on June 6, 2012).The entire t...
This thesis is on computational fluid-structure interaction (FSI) modeling of bioinspired flapping-w...
AbstractTo evaluate the propulsion system capabilities of a Flapping Micro Air Vehicle (FMAV), a new...
This paper discusses a methodology of analyzing the flight dynamic stability of a flapping wing Micr...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...