Structural design and experimental verification of a novel split aileron wing
Many unmanned aerial vehicles (UAVs) such as solar powered ones require their top
surfaces of the wings to be integral and gap free. To enable rolling movement and improve …
surfaces of the wings to be integral and gap free. To enable rolling movement and improve …
Yaw stability analysis for UiTM's BWB baseline-II UAV E-4
This paper presents a study about yaw stability analysis for UiTMs Blended-Wing-Body
(BWB) Baseline-II E-4. This aircraft is equipped with split drag flaps in order to perform …
(BWB) Baseline-II E-4. This aircraft is equipped with split drag flaps in order to perform …
A study about the split drag flaps deflections to directional motion of UiTM's blended wing body aircraft based on computational fluid dynamics simulation
This paper discusses on the split drag flaps to the yawing motion of BWB aircraft. This study
used split drag flaps instead of vertical tail and rudder with the intention to generate yawing …
used split drag flaps instead of vertical tail and rudder with the intention to generate yawing …
Structural design and aerodynamic characteristic of an innovative split aileron configuration
An innovative design scheme of the aileron configuration, called no assembled gap of
trailing-edge of the wing, uses split aileron that hat is located on the under surface of the …
trailing-edge of the wing, uses split aileron that hat is located on the under surface of the …
[PDF][PDF] A Study about the Split Drag Flaps Deflections to Directional Motion of UiTM's BWB Aircraft Based on CFD Simulation
This paper discusses on the split drag flaps to the yawing motion of BWB aircraft. This study
used split drag flaps instead of vertical tail and rudder with the intention to generate yawing …
used split drag flaps instead of vertical tail and rudder with the intention to generate yawing …