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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 …
has been undertaken to elucidate the deformation of an axisymmetric jet (ReD≈ 1950 and …
Large-and small-scale vortical motions in a shear layer perturbed by tabs
JK Foss, K Zaman - Journal of Fluid Mechanics, 1999 - cambridge.org
The large-and small-scale vortical motions produced by 'delta tabs' in a two-stream shear
layer have been studied experimentally. An increase in mixing was observed when the base …
layer have been studied experimentally. An increase in mixing was observed when the base …
Experimental studies on the limiting tab
E Rathakrishnan - AIAA Journal, 2009 - arc.aiaa.org
DESIGN of large and fast jet-propelled aircraft and large booster rocket engines have
focused on noise problems. Difficulties in devising satisfactory solutions stem from the …
focused on noise problems. Difficulties in devising satisfactory solutions stem from the …
Experimental study on enhancement of supersonic twin-jet mixing by vortex generators
Experimental results on the mean flow evolution and the control of single and twin
compressible jets at Mach 1.6 are presented. The jets issue from conical CD nozzles closely …
compressible jets at Mach 1.6 are presented. The jets issue from conical CD nozzles closely …
Corrugated tabs for supersonic jet control
BC Phanindra, E Rathakrishnan - AIAA journal, 2010 - arc.aiaa.org
Pc= pitot pressure Pe= nozzle exit pressure P0= setting chamber pressure R= distance
along the radial direction for uncontrolled jets X= axial distance along the x-axis x …
along the radial direction for uncontrolled jets X= axial distance along the x-axis x …
Numerical investigation of very low reynolds cross orifice jet for personalized ventilation applications in aircraft cabins
This study focuses on the numerical analysis of a challenging issue involving the regulation
of the human body's microenvironment through personalized ventilation. We intended to first …
of the human body's microenvironment through personalized ventilation. We intended to first …
Flow structures of a lobed mixer and effects of streamwise vortices on mixing enhancement
X Fang, C Shen, M Sun, RD Sandberg, P Wang - Physics of Fluids, 2019 - pubs.aip.org
Large-scale vortices downstream of a lobed mixer are investigated experimentally using a
nanoparticle-based planar laser scattering experimental system. The results are contrasted …
nanoparticle-based planar laser scattering experimental system. The results are contrasted …
Supersonic jet flow control using semi-circular corrugated tabs
S Chidambaram - Aircraft Engineering and Aerospace Technology, 2019 - emerald.com
Purpose The purpose of this study is to increase the jet mixing effectiveness of Mach 1.6
axisymmetric jet using semi-circular corrugated triangular tabs (Tabs A, B and C), in which …
axisymmetric jet using semi-circular corrugated triangular tabs (Tabs A, B and C), in which …
Truncated triangular tabs for supersonic-jet control
PA Kumar, E Rathakrishnan - Journal of Propulsion and Power, 2013 - arc.aiaa.org
An experimental investigation has been carried out to study the mixing-promoting efficiency
of triangular tabs with sharp and truncated vertices. The mixing promotion caused by two …
of triangular tabs with sharp and truncated vertices. The mixing promotion caused by two …
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 …
vertex has been investigated by placing two identical tabs at the exit of a Mach 2 axi …