Unsteady aerodynamics of a morphing tandem-wing unmanned aerial vehicle
The effects of unsteady aerodynamics for a tandem-wing unmanned aerial vehicle (UAV) prototype during the morphing stage have been investigated numerically at low Reynolds numbers (Re<10^6). The morphing stage consists of two stages. The first stage involves the unfolding of the canards and wings...
Saved in:
Main Authors: | Zhang, G. Q., Yu, S. C. M. |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Article |
Language: | English |
Published: |
2013
|
Online Access: | https://hdl.handle.net/10356/85676 http://hdl.handle.net/10220/11677 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Unsteady aerodynamic investigation of the propeller-wing interaction for a rocket launched unmanned air vehicle
by: Zhang, G. Q., et al.
Published: (2013) -
Unsteady Aerodynamics of Flapping Wings
by: ZHANG LIUHANG
Published: (2013) -
Propeller-induced effects on the aerodynamics of a small unmanned aerial vehicle
by: Maqsood, Adnan, et al.
Published: (2013) -
UNSTEADY AERODYNAMICS OF FLAPPING WING: GROUND EFFECT AND ROTATIONAL LIFT
by: LU HAO
Published: (2015) -
Assembly of fixed wing Unmanned Aerial Vehicle (UAVs)
by: Low, Daniel Wen Jian.
Published: (2013)