Investigation of the tail dihedral effects on the aerodynamic characteristics for the low speed aircraft
The aerodynamic characteristics for the vee-tail aircraft configuration have been investigated numerically at low Reynolds number (Re < 10 6). Three types of vee-tails have been adopted to be compared with the conventional tail type (with horizontal and vertical tails).The results show that th...
Saved in:
Main Authors: | Zhang, G. Q., Yu, S. C. M., Chien, A., Xu, Y. |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Article |
Language: | English |
Published: |
2014
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/85689 http://hdl.handle.net/10220/18654 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Design and sizing eVTOL aircraft (aerodynamics portion)
by: Dikshit, Abhijnan
Published: (2022) -
Unsteady aerodynamic investigation of the propeller-wing interaction for a rocket launched unmanned air vehicle
by: Zhang, G. Q., et al.
Published: (2013) -
Aerodynamic characteristics of the ventilated design for flapping wing micro air vehicle
by: Zhang, G. Q., et al.
Published: (2014) -
Experimental and numerical investigations on the aerodynamics of a simplified helicopter fuselage
by: Cheawchan, Atcha-uea
Published: (2022) -
Aerodynamics investigation of MAV with flexible wing
by: Zeng, Zibin
Published: (2011)