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Shock structures of underexpanded non-circular slot jets

TLDR
In this article, the authors used shadowgraph technique to investigate the shock evolution from non-circular slot jets at various underexpansion levels and found that the shock cell structures of noncircular jets strongly depend upon the initial shape of the topology.
Abstract
Flow visualization studies using shadowgraph technique are carried out to investigate the shock evolution from non-circular slot jets at various under-expansion levels. The non-circular topologies considered are triangular, square and elliptic, and the circular jet is taken as the baseline case for the study. These jets are underexpanded in the pressure ratio (R) range of 2–6 corresponding to a fully expanded jet Mach number up to 1.85. Results indicate that the shock cell structures of non-circular jets strongly depend upon the initial shape of the topology. The shock structures of triangular jet have additional secondary oblique shocks that are distinct from those of other non-circular jets. Mach disk is almost absent in a shock cell structure of triangular jet, which is unlike the case of other jets used in the study. The study suggests that square jet undergoes faster diffusion process compared with the triangular jet. Axis-switching phenomenon is predicted for the elliptical jet at a distance of 3–7 equivalent diameters.

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Numerical investigations on pilot ignited high pressure direct injection natural gas engines: A review

TL;DR: In this paper, numerical investigations concerning underexpanded gas jets and in-cylinder working process of pilot ignited high pressure direct injection natural gas engines are involved, and different numerical models adopted in the previous studies are systematically evaluated.
Journal ArticleDOI

Schlieren imaging investigation on azimuthally varying shock net from four-lobed corrugated nozzle

TL;DR: In this paper , the Schlieren images were captured for seven different nozzle pressure ratios (NPR = 2, 3, 4, 5, 6, 7 and 8) and compared with the shock cell structure of a round nozzle with an identical exit area.
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Effects of circular and non-circular nozzle exit geometries on subsonic and supersonic jet propagations

TL;DR: In this paper , the effects of two non-circular nozzle exit shapes (elliptic and square) on the mixing augmenting efficacy at subsonic and sonic flow conditions were examined.
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Numerical investigation of the cryogenic underexpanded hydrogen jets exiting rectangular shaped openings

TL;DR: In this paper , a numerical model of underexpanded jets was employed to evaluate the effect of jet temperature and aspect ratio of rectangular nozzles on the shock structure and dispersion characteristics.
References
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Journal ArticleDOI

The compressible turbulent shear layer: an experimental study

TL;DR: In this paper, the growth rate and turbulent structure of the compressible, plane shear layer are investigated experimentally in a novel facility, where it is possible to flow similar or dissimilar gases of different densities and to select different Mach numbers for each stream.
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On the Mechanism of Choked Jet Noise

TL;DR: In this paper, the authors examined the noise in two-dimensional flow with the aid of a dynamic Schlieren apparatus, verifying the suggested mechanism and showing the similarity to axially symmetric flow where discontinuities in frequency, partly analogous to edge tones, occur.
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Flow control with noncircular jets

TL;DR: Noncircular jets have been identified as an efficient technique of passive flow control that allows significant improvements of performance in various practical systems at a relatively low cost because noncircular jet rely solely on changes in the geometry of the nozzle as discussed by the authors.
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Vortex induction and mass entrainment in a small-aspect-ratio elliptic jet

TL;DR: In this article, a passive technique of increasing entrainment was found by using a small-aspect-ratio elliptic jet, which was several times greater than that of a circular jet or a plane jet.
Journal ArticleDOI

Two-dimensional shear-layer entrainment

TL;DR: In this article, a simple argument is proposed, based on the geometrical properties of the large-scale now structures of the subsonic, fully developed, two-dimensional mixing layer, which yields the entrainment ratio and growth of the turbulent mixing layer.
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