Aerodynamic Optimization Design of Duct Body Structure for Coaxial Rotor Unmanned Aerial Vehicles
With the rapid development of vertical takeoff and landing aircraft, urban air traffic has gradually attracted people’s attention. The lift system is a key technology in the composition of vertical takeoff and landing aircraft systems. Due to its compact structure, low noise, safety, and reliability...
Saved in:
Main Authors: | Du Siliang, Zha Yi, Zhao Qijun |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2024-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2024/2295279 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Aerodynamics Optimization of a Ducted Coaxial Rotor in Forward Flight Using Orthogonal Test Design
by: Yuening Jiang, et al.
Published: (2018-01-01) -
Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System
by: Xueqiang Shen, et al.
Published: (2018-01-01) -
Aerodynamic and Inertial Loading Effects of Insect-Inspired Appendages in Small Unmanned Aerial Vehicles
by: Titilayo Ogunwa, et al.
Published: (2025-01-01) -
Detection and identification technology of rotor unmanned aerial vehicles in 5G scene
by: Fengtong Xu, et al.
Published: (2019-06-01) -
Aerodynamic Interaction Characteristics Study of the Ducted Coaxial Propeller for a Novel eVTOL in Hovering
by: Junjie Wang, et al.
Published: (2023-01-01)