Direct numerical simulations (DNS) of laminar separation bubbles on a NACA-0012 airfoil at
Rec= 5× 104 and incidence 5° are presented. Initially volume forcing is introduced in order …

A pair of oblique waves at low amplitudes is introduced in a supersonic flat-plate boundary
layer at Mach 3. Its downstream development and the concomitant process of laminar to …

The role of free-stream turbulence (FST) in the hydrodynamic instability mechanisms and
transition to turbulence in laminar separation bubbles (LSBs) was investigated using direct …

The transition process in a supersonic flat-plate boundary layer at Mach 2 is investigated
numerically using linear stability theory (LST) and direct numerical simulations (DNS). The …

Our previous research has shown that an active flow control strategy using two-dimensional
(2-D) harmonic blowing and suction with properly chosen frequency and amplitude can …

A flow simulation Methodology (FSM) is presented for computing the time-dependent
behavior of complex compressible turbulent flows. The development of FSM was initiated in …

In the present study, numerical simulations of two-dimensional steady-state incompressible
Newtonian fluid flow in one-sided and four-sided lid-driven square cavities are reported. For …

The quasi-two-dimensional flow of a liquid metal subjected to a strong transverse magnetic
field around a 180-degree sharp bend is investigated by means of parametric numerical …

WHEN considering airfoil self-noise most studies focus upon trailing-edge noise. Indeed,
Brooks et al.[1] classified five mechanisms for airfoil self-noise, all but one of which have …

Direct numerical simulation data of supersonic axisymmetric wakes are analysed for the
existence of large coherent structures. Wakes at Ma= 2.46 are considered with results being …