The control of bluff-body wakes for reduced drag and enhanced stability has traditionally
relied on the so-called direct-wake control approach. By the use of actuators or passive …

Amplitude scaling laws for active control of boundary layer separation using discrete jet
forcing are not fully established. Momentum coefficient is the most widely accepted scaling …

Prandtl in 1904 [1] and, in particular, the control of boundary-layer separation. Traditional
boundary layer control (BLC) involved the addition of momentum flux or the removal of the …

This paper presents an experimental study on the effects of the Reynolds number (Re sj=
300, 600, and 900) and porosity (ϕ= 20%–85%) on synthetic jet vortex rings impinging onto …

Current research in hypersonic wind tunnel aerodynamic testing predominantly focuses on
small-scale and lightweight models, typically limited to scales of 4 m and weights under 1 …

This work investigates the wake behind an axisymmetric bluff body at R e D∼ 2⋅ 1 0 5 and
applies control via four types of travelling jets which consist of different jet profiles …

The coherent structures of a turbulent axisymmetric bluff body wake are investigated based
on synchronised near-wake velocity and base pressure measurements. The proper …

Integrated airframe/propulsion aerodynamic tests in a hypersonic wind tunnel are critical for
developing an air-breathing hypersonic vehicle. Spurred by the shortcomings of traditional …

A data-driven method using Grassmann manifold learning is proposed to identify a low-
dimensional actuation manifold for flow-controlled fluid flows. The snapshot flow field are …

Modern advanced fighters are characterized by the post-stall maneuverability with multi-
degree-of-freedom (M-DOF) at high angles of attack (AoAs), which is generally difficult to …