A review of jet mixing enhancement for aircraft propulsion applications

K Knowles, AJ Saddington - Proceedings of the Institution of …, 2006 - journals.sagepub.com
This article reviews techniques applicable to enhancing the mixing of jets, with particular
emphasis on infrared (IR) signature reduction of high-speed jets. Following a brief …

Structure of a particle-laden round jet

EK Longmire, JK Eaton - Journal of Fluid Mechanics, 1992 - cambridge.org
The interaction of solid particles with the temporal features of a turbulent flow has direct
relevance to problems in particle and spray combustion and the processing of particulate …

The evolution of a jet with vortex-generating tabs: real-time visualization and quantitative measurements

MF Reeder, M Samimy - Journal of Fluid mechanics, 1996 - cambridge.org
An experimental study involving flow visualization and two-component LDV measurements
has been undertaken to elucidate the deformation of an axisymmetric jet (ReD≈ 1950 and …

Mixing processes in a coaxial geometry with a central lobed mixer-nozzle

VM Belovich, M Samimy - AIAA journal, 1997 - arc.aiaa.org
An experimental investigation was undertaken to study mixing processes in a coaxial jet,
where the inner jet geometry is a lobed mixer. Various inner jet nozzle geometries were …

[PDF][PDF] Jet noise reduction technology development at GE aircraft engines

S Martens - ICAS paper, 2002 - icas.org
Several years ago, GE Aircraft Engines realized that with the expected increased stringency
of Stage 4 noise regulations, the continued thrust growth of engine families, and increasing …

Spatial evolution of multi-scale droplet clusters in an evaporating spray

N Pandurangan, S Sahu - Physics of Fluids, 2022 - pubs.aip.org
Evaporative sprays are encountered in a wide range of engineering applications. Since
clustering of droplets in sprays leads to strong inhomogeneity in the spatial distribution of …

Noise, turbulence, and thrust of subsonic freejets from lobed nozzles

K Zaman, FY Wang, NJ Georgiadis - AIAA journal, 2003 - arc.aiaa.org
A study of noise bene t, vis-a-vis thrust penalty, and its correlation to turbulence intensities is
conducted for freejets issuing from lobed nozzles. Four convergent nozzles with constant …

AST critical propulsion and noise reduction technologies for future commercial subsonic engines: separate-flow exhaust system noise reduction concept evaluation

BA Janardan, GE Hoff, JW Barter, S Martens… - 2000 - ntrs.nasa.gov
This report describes the work performed by General Electric Aircraft Engines (GEAE) and
Allison Engine Company (AEC) on NASA Contract NAS3-27720 AoI 14.3. The objective of …

Mixing enhancement via nozzle trailing edge modifications in a high speed rectangular jet

JH Kim, M Samimy - Physics of Fluids, 1999 - pubs.aip.org
An aspect ratio 3 rectangular nozzle with design Mach number 2 was used to investigate the
effects of trailing edge modifications on mixing enhancement and to explore the sources of …

Triangular tabs for supersonic jet mixing enhancement

A Kumar, E Rathakrishnan - The Aeronautical Journal, 2014 - cambridge.org
The mixing promoting capability of right-angled triangular tab with sharp and truncated
vertex has been investigated by placing two identical tabs at the exit of a Mach 2 axi …