1991
DOI: 10.2514/3.23317
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Subsonic and supersonic combustion using noncircular injectors

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Cited by 69 publications
(32 citation statements)
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“…The higher turbulence intensities at the corners of the triangular and rectangular nozzles have been shown by [19] to produce a stronger vortex pair which enhances entrainment and spreading rates. There are different scales of turbulence for the asymmetric nozzles according to [12]. The small-scale structures occur at the nozzle corners and the large-scale structures at the flat sides [12].…”
Section: Development Of the Jet Half-velocity Width With The Presencementioning
confidence: 99%
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“…The higher turbulence intensities at the corners of the triangular and rectangular nozzles have been shown by [19] to produce a stronger vortex pair which enhances entrainment and spreading rates. There are different scales of turbulence for the asymmetric nozzles according to [12]. The small-scale structures occur at the nozzle corners and the large-scale structures at the flat sides [12].…”
Section: Development Of the Jet Half-velocity Width With The Presencementioning
confidence: 99%
“…Furthermore, Zaman [20], and Gutmark and co-workers [7][8][9] reported discrepancies concerning the extent of the increase in jet spreading and entrainment of rectangular nozzles as opposed to circular nozzles. Indeed, while Gutmark and co-workers [10][11][12] observed considerable increase in jet spreading and entrainment of the rectangular nozzles (with an aspect ratio of 2:1) compared to their circular nozzle counterpart, Zaman [20], who performed an experiment at a much higher Reynolds number (i.e. compressible flow) observed only slight increase for the same geometry.…”
mentioning
confidence: 90%
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“…Gutmark et al [21,22] compared the mixing characteristics between the circular, elliptic and rectangular jets from the subsonic flow to supersonic flow, and found that the elliptic and rectangular jets had a higher spreading rate relative to the circular jet, especially at the minor axis plane. After that, there have been some efforts [23][24][25][26][27][28] devoted to directly comparing the flow properties between the underexpanded jets issuing from different nozzle geometries.…”
Section: Introductionmentioning
confidence: 99%
“…In partially nonpremixed flames, except in the near-burner region, the local air-fuel ratio depends upon the air-infusion rate into the burning jet, which can be controlled either by changing the flow dynamics or manipulating the downstream flow characteristics of the gas jet. The application of non-axisymmetric burner exit geometries (Gollahalli et al, 1992;Gutmark et al,1991;Schadow et al, 1989;Kamal and Gollahalli, 1993;Papanikolau and Wierzba, 1996;Papanikolau et al, 1997) is an example of such a technique that showed some improvements in the combustion and emission characteristics of burning gas jets.…”
Section: Introductionmentioning
confidence: 99%