Paper
1 December 2021 Wing flexibility effects in micro air vehicle performance
Author Affiliations +
Proceedings Volume 12079, Second IYSF Academic Symposium on Artificial Intelligence and Computer Engineering; 120791C (2021) https://doi.org/10.1117/12.2622872
Event: 2nd IYSF Academic Symposium on Artificial Intelligence and Computer Engineering, 2021, Xi'an, China
Abstract
The content of this simulation is the influence of rigidity and flexibility on the aerodynamic performance of airfoil. The research objects are drones and rotors. The focus is on rotors with different speeds of rigid rotors, different speeds of flexible rotors, and different elastic moduli (stiffness) of flexible rotors. Research on lift and torque.
© (2021) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Lei Chu "Wing flexibility effects in micro air vehicle performance", Proc. SPIE 12079, Second IYSF Academic Symposium on Artificial Intelligence and Computer Engineering, 120791C (1 December 2021); https://doi.org/10.1117/12.2622872
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Solids

Aerodynamics

3D modeling

Micro unmanned aerial vehicles

Unmanned aerial vehicles

Aerospace engineering

Mechanics

Back to Top