Experimental Investigation into the Aerodynamic Properties of a Flexible and Rigid Wing Micro AIr Vehicle

2004 ◽  
Author(s):  
Anthony DeLuca ◽  
Mark Reeder ◽  
Michael Ol ◽  
Jacob Freeman ◽  
Michael Simonich ◽  
...  
Keyword(s):  
Experimental Investigation ◽  
Micro Air Vehicle ◽  
Aerodynamic Properties ◽  
Air Vehicle ◽  
Rigid Wing

scholarly journals Experimental Investigation of Micro Air Vehicle Scale Helicopter Rotor in Hover

2015 ◽  
Vol 7 (3) ◽  
pp. 231-255 ◽  
Author(s):  
Moble Benedict ◽  
Justin Winslow ◽  
Zohaib Hasnain ◽  
Inderjit Chopra
Keyword(s):  
Experimental Investigation ◽  
Micro Air Vehicle ◽  
Helicopter Rotor ◽  
Air Vehicle

Flexible- and Rigid-Wing Micro Air Vehicle: Lift and Drag Comparison

2006 ◽  
Vol 43 (2) ◽  
pp. 572-575 ◽  
Author(s):  
Anthony M. DeLuca ◽  
Mark F. Reeder ◽  
Jacob A. Freeman ◽  
Michael V. Ol
Keyword(s):  
Micro Air Vehicle ◽  
Air Vehicle ◽  
Lift And Drag ◽  
Rigid Wing

scholarly journals Experimental Investigation on the Aerodynamics of a Bio-Inspired Flexible Flapping Wing Micro Air Vehicle

2014 ◽  
Vol 6 (2) ◽  
pp. 105-115 ◽  
Author(s):  
Shuanghou Deng ◽  
Mustafa Percin ◽  
Bas van Oudheusden ◽  
Bart Remes ◽  
Hester Bijl
Keyword(s):  
Experimental Investigation ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Air Vehicle

scholarly journals Experimental investigation of wing flexibility on force generation of a hovering flapping wing micro air vehicle with double wing clap-and-fling effects

2017 ◽  
Vol 9 (3) ◽  
pp. 187-197 ◽  
Author(s):  
Quoc V Nguyen ◽  
Woei L Chan ◽  
Marco Debiasi
Keyword(s):  
Experimental Investigation ◽  
Power Consumption ◽  
High Speed ◽  
Electrical Power ◽  
Leading Edge ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Custom Made ◽  
Air Vehicle ◽  
Set Up

Experimental investigation of wing flexibility on vertical thrust generation and power consumption in hovering condition for a hovering Flapping-Wing Micro Air Vehicle, namely FlowerFly, weighing 14.5 g with a 3 g onboard battery and having four wings with double wing clap-and-fling effects, was conducted for several wing configurations with the same shape, area, and weight. A data acquisition system was set up to simultaneously record aerodynamic forces, electrical power consumption, and wing motions at various flapping frequencies. The forces and power consumption were measured with a loadcell and a custom-made shunt circuit, respectively, and the wing motion was captured by high-speed cameras. The results show a phase delay of the wing tip displacement observed for wings with high flexible leading edge at high frequency, resulting in less vertical thrust produced when compared with the wings with less leading edge flexibility at the same flapping frequency. Positive wing camber was observed during wing flapping motion by arranging the wing supporting ribs. Comparison of thrust-to-power ratios between the wing configurations was undertaken to figure out a wing configuration for high vertical thrust production but less power consumption.

Experiments on Rigid Wing Undergoing Hover-Capable Flapping Kinematics at Micro-Air-Vehicle-Scale Reynolds Numbers

AIAA Journal ◽  
2016 ◽  
Vol 54 (4) ◽  
pp. 1145-1157 ◽  
Author(s):  
Moble Benedict ◽  
David Coleman ◽  
David B. Mayo ◽  
Inderjit Chopra
Keyword(s):  
Reynolds Numbers ◽  
Micro Air Vehicle ◽  
Air Vehicle ◽  
Rigid Wing
Sign in / Sign up

Export Citation Format

Share Document