The ground effect influences the flow structure on a delta wing during landing and take-off
processes. In this regard, comprehensive instantaneous velocity measurements and flow …

The stall characteristics of the cuspidal waverider under subsonic conditions were studied at
M= 0.4 and H= 0 km incoming flow. The stall characteristics were compared with those of …

The dynamic modelling and attitude controller design of a flapping wing aircraft, Beihawk,
were investigated in this study. The aircraft features of an X-shaped flapping wing …

High-pressure capturing wing (HCW) configuration is a potential hypersonic aerodynamic
configuration that can simultaneously have good lift-drag characteristics with a large …

For complicated unsteady separated flow problem of slender body at extra-wide of angle of
attack range, delayed detached eddy simulation based on shear stress transport turbulence …

The pitching oscillations (α from 0° to 60°) of a close-coupled coplanar canard configuration
were investigated at various reduced frequencies (k= 0.0375, 0.075, 0.15, 0.3, 0.6 and 1.2) …

In this research, the effect of the leading-edge extension (LEX) angle on the flow pattern
upstream and downstream of the diamond wing has been investigated experimentally. The …

The flow control effect of Gurney flaps on 50° swept delta wings during large-amplitude and
high-frequency pitching were investigated both experimentally and numerically. Both force …

The use of flow control techniques is important to enhance vehicle motion stability during
water entry. This paper introduces a method that applies a canard wing to the water entry …

This paper considers a novel multi-degree-of-freedom dynamic manoeuvre rig, with the aim
of assessing its potential for capturing aircraft model nonlinear time dependent dynamics in …