scholarly journals Preliminary Design and Computational Fluid Dynamic analysis of Flapping Wing of Micro Aerial Vehicle for Low Reynolds Numbers Regime

2019 ◽  
Vol 1 (2) ◽  
pp. 36-45
Author(s):  
Abduljaleel Altememe ◽  
Oliver J Myers ◽  
Asha Hall
Keyword(s):  
Dynamic Analysis ◽  
Computational Fluid Dynamic ◽  
Fluid Dynamic ◽  
Reynolds Numbers ◽  
Flapping Wing ◽  
Preliminary Design ◽  
Computational Fluid Dynamic Analysis ◽  
Micro Aerial Vehicle ◽  
Low Reynolds Numbers ◽  
Aerial Vehicle

Preliminary Design of Flapping Wing Micro Aerial Vehicle at Low Reynolds Numbers

2016 ◽  
Author(s):  
Abduljaleel Altememe ◽  
Stanley Anderson ◽  
Oliver J. Myers ◽  
Asha J. Hall
Keyword(s):  
Reynolds Numbers ◽  
Flapping Wing ◽  
Preliminary Design ◽  
Biologically Inspired ◽  
Micro Aerial Vehicle ◽  
Low Reynolds Numbers ◽  
Gas Detectors ◽  
Aerial Vehicle ◽  
Low Reynolds ◽  
Critical Components

This research discusses preliminary design of a Flapping Wing Micro Aerial Vehicle (FWMAV). One approach is to develop a biologically-inspired flapping wing MAV that can maneuver into confined areas and possess hover capabilities. This platform can potentially be equipped with microphones, cameras, and gas detectors, but one major challenge is the low Reynolds number aerodynamics. The critical components for successful flight include size, weight, and energy efficiency. Preliminary efforts include mechanical designs for payload, biologically inspired chassis, wing and tail.

Computational fluid dynamic analysis at dam spillway due to different gate openings

2018 ◽  
Author(s):  
M. H. Zawawi ◽  
N. A. Aziz ◽  
M. R. M. Radzi ◽  
N. H. Hassan ◽  
M. Z. Ramli ◽  
...  
Keyword(s):  
Dynamic Analysis ◽  
Computational Fluid Dynamic ◽  
Fluid Dynamic ◽  
Computational Fluid Dynamic Analysis
Sign in / Sign up

Export Citation Format

Share Document