Wind tunnel testing of hybrid buoyant aerial vehicle
Purpose – Realistic data bank of aerodynamic and stability derivatives is still missing for hybrid buoyant aerial vehicles. Such vehicles take-off and land similar to an aircraft with their partial weight balanced by the aerostatic lift. The purpose of this paper is to use wind tunnel testing for a...
| Main Authors: | UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Ali, JS Mohamed |
|---|---|
| Format: | Article |
| Language: | English English English |
| Published: |
Emerald Publishing Limited
2017
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/55356/ http://irep.iium.edu.my/55356/ http://irep.iium.edu.my/55356/ http://irep.iium.edu.my/55356/1/55356_Wind%20tunnel%20testing%20of%20hybrid.pdf http://irep.iium.edu.my/55356/2/55356-Wind%20tunnel%20testing%20of%20hybrid%20buoyant_SCOPUS.pdf http://irep.iium.edu.my/55356/3/55356_Wind%20tunnel%20testing%20of%20hybrid_WOS.pdf |
Similar Items
-
Yawing force of electric trimmers of a hybrid buoyant aerial vehicle
by: UlHaque, Anwar, et al.
Published: (2017) -
Effect of side wind on the directional stability and aerodynamics of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016) -
Wind tunnel testing on a generic model of a hybrid lifting hull
by: UlHaque, Anwar, et al.
Published: (2016) -
Stability and takeoff ground roll issues of hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2014) -
Assessment of engine's power budget for hydrogen
powered hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)