Review of combustion stabilization for hypersonic airbreathing propulsion
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
Modern developments in flow control
M Gad-el-Hak - 1996 - asmedigitalcollection.asme.org
This brief article reviews the important advances in the field of flow control that took place
during the past few years. This broad area of research remains of great interest for its …
during the past few years. This broad area of research remains of great interest for its …
[BOOK][B] Flow control
M Gad-el-Hak - 2000 - ui.adsabs.harvard.edu
The ability to actively or passively manipulate a flow field to bring about a desired change is
of immense technological and economical importance. This volume provides a thorough, up …
of immense technological and economical importance. This volume provides a thorough, up …
Active control of high-speed and high-Reynolds-number jets using plasma actuators
Localized arc filament plasma actuators are used to control an axisymmetric Mach 1.3
ideally expanded jet of 2.54 cm exit diameter and a Reynolds number based on the nozzle …
ideally expanded jet of 2.54 cm exit diameter and a Reynolds number based on the nozzle …
Supersonic jet screech: half-century from Powell to the present
G Raman - Journal of Sound and Vibration, 1999 - Elsevier
Under certain conditions, shock-containing jets produce an intense tone referred to as
screech. Screech was discovered about half a century ago by Alan Powell in England. Here …
screech. Screech was discovered about half a century ago by Alan Powell in England. Here …
Spreading characteristics of compressible jets from nozzles of various geometries
K Zaman - Journal of Fluid mechanics, 1999 - cambridge.org
The spreading characteristics of jets from several asymmetric nozzles, and a set of
rectangular orifices are compared, covering a jet Mach number range of 0.3–2.0. The effect …
rectangular orifices are compared, covering a jet Mach number range of 0.3–2.0. The effect …
Shock wave—turbulence interactions
Y Andreopoulos, JH Agui… - Annual review of fluid …, 2000 - annualreviews.org
▪ Abstract The idealized interactions of shock waves with homogeneous and isotropic
turbulence, homogeneous sheared turbulence, turbulent jets, shear layers, turbulent wake …
turbulence, homogeneous sheared turbulence, turbulent jets, shear layers, turbulent wake …
Compressibility effects in a turbulent annular mixing layer. Part 1. Turbulence and growth rate
This work uses direct numerical simulations of time evolving annular mixing layers, which
correspond to the early development of round jets, to study compressibility effects on …
correspond to the early development of round jets, to study compressibility effects on …
Advances in understanding supersonic jet screech: review and perspective
G Raman - Progress in aerospace sciences, 1998 - Elsevier
Screech tones are produced by imperfectly expanded jets under certain conditions. This
paper provides an overview of developments in the field of supersonic jet screech. The …
paper provides an overview of developments in the field of supersonic jet screech. The …
Review of theoretical modelling approaches of Rayleigh–Taylor instabilities and turbulent mixing
SI Abarzhi - … Transactions of the Royal Society A …, 2010 - royalsocietypublishing.org
We review the theoretical developments in the field of Rayleigh–Taylor instabilities and
turbulent mixing, discuss what is known and what is not known about the phenomenon, and …
turbulent mixing, discuss what is known and what is not known about the phenomenon, and …