In this paper we present preliminary results from a high-resolution large eddy simulation (LES) study which will establish whether jet inlet velocity conditions are of significance in separation control applications. We include orifice geometry, in order to allow realistic turbulent structures to naturally develop. Ultimately, we will simulate various momentum thicknesses, (D/theta= 50, 80, 120 and 180) at Rej = 104 where Rej = UjD/nu, where Uj is the jet inflow velocity and D is the jet diameter, however this paper presents initial high-resolution LES results for a steady jet, Rej = 104, D/theta = 50. The 1:2 x10^7 cell model was computed using the iVEC EPIC supercomputing cluster, and our local Beowulf cluster at Curtin University, (12 x ...
Large-Eddy Simulation (LES) was originally proposed for simulating atmospheric flows in the 1960s an...
The paper presents Large Eddy Simulations (LES) of mass transfer and fluid flow evolutions of a subm...
Computations are made of a short cowl coflowing jet nozzle with a bypass ratio 8 : 1. The core flow ...
Abstract: In this paper we present preliminary results from a high-resolution large eddy simulation ...
In this paper we present preliminary results from a high-resolution large eddy simulation (LES) stud...
The current research focuses on the use of synthetic jets with a rectangular orifice of high aspect ...
The effect of a cross-sectional exit plane on the downstream mixing characteristics of a circular tu...
For jets, large eddy resolving simulations are compared for a range of numerical schemes with no sub...
A complete understanding of the noise generation mechanisms is prerequisite to reducing aircraft jet...
International audienceThe present study is concerned with large-eddy simulations (LES) of supersonic...
This thesis deals with Large Eddy Simulation (LES) of impinging air jets. The impinging jet configur...
This paper reviews the current state of large-eddy simulation (LES) for nozzle flows and discusses t...
Computations are made for chevron and coflowing jet nozzles. The latter has a bypass ratio of 6:1. A...
A large-eddy simulation (LES) of a compressible nozzle/jet configuration has been carried out. A col...
A Large-Eddy Simulation (LES) investigation was performed with the aim of analysing flow behaviour i...
Large-Eddy Simulation (LES) was originally proposed for simulating atmospheric flows in the 1960s an...
The paper presents Large Eddy Simulations (LES) of mass transfer and fluid flow evolutions of a subm...
Computations are made of a short cowl coflowing jet nozzle with a bypass ratio 8 : 1. The core flow ...
Abstract: In this paper we present preliminary results from a high-resolution large eddy simulation ...
In this paper we present preliminary results from a high-resolution large eddy simulation (LES) stud...
The current research focuses on the use of synthetic jets with a rectangular orifice of high aspect ...
The effect of a cross-sectional exit plane on the downstream mixing characteristics of a circular tu...
For jets, large eddy resolving simulations are compared for a range of numerical schemes with no sub...
A complete understanding of the noise generation mechanisms is prerequisite to reducing aircraft jet...
International audienceThe present study is concerned with large-eddy simulations (LES) of supersonic...
This thesis deals with Large Eddy Simulation (LES) of impinging air jets. The impinging jet configur...
This paper reviews the current state of large-eddy simulation (LES) for nozzle flows and discusses t...
Computations are made for chevron and coflowing jet nozzles. The latter has a bypass ratio of 6:1. A...
A large-eddy simulation (LES) of a compressible nozzle/jet configuration has been carried out. A col...
A Large-Eddy Simulation (LES) investigation was performed with the aim of analysing flow behaviour i...
Large-Eddy Simulation (LES) was originally proposed for simulating atmospheric flows in the 1960s an...
The paper presents Large Eddy Simulations (LES) of mass transfer and fluid flow evolutions of a subm...
Computations are made of a short cowl coflowing jet nozzle with a bypass ratio 8 : 1. The core flow ...