2013
DOI: 10.4236/jfcmv.2013.13012
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Stability of Subsonic Jet Flows

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Cited by 12 publications
(7 citation statements)
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“…These shear layer structures also became more organized as the jet density was reduced relative to the density of the ambient gas [8]. Both the flow dynamics and possible instabilities in the jet strongly depend on the conditions at the nozzle exit including the Reynolds number, nozzle geometry and initial velocity [6,11]. Hence it is often difficult to make general conclusions on flow structures of different jets.…”
Section: Introductionmentioning
confidence: 99%
“…These shear layer structures also became more organized as the jet density was reduced relative to the density of the ambient gas [8]. Both the flow dynamics and possible instabilities in the jet strongly depend on the conditions at the nozzle exit including the Reynolds number, nozzle geometry and initial velocity [6,11]. Hence it is often difficult to make general conclusions on flow structures of different jets.…”
Section: Introductionmentioning
confidence: 99%
“…The flame behaviour is correlated with the process of round free jet flattening and bifurcation in a transverse acoustic field [6]. Acoustic forcing of a slit burner flame was experimentally investigated in [5], and it was confirmed that the bifurcation of the jet due to acoustic forcing is basically a two-dimensional phenomenon.…”
Section: Diffusion Combustion Of Propane Round Microjetmentioning
confidence: 99%
“…However, this mechanism still remains unclear. The experimental studies [6][7][8][9][10][11][12] and other, where the influence of the initial conditions at the nozzle exit and acoustics on the development of round and plane microjets in the absence of combustion at low Reynolds numbers were investigated in detail, which made it possible to understand and explain some phenomena in the flame behaviour observed during propane combustion in these jets. The results of these studies are presented in this paper.…”
Section: Introductionmentioning
confidence: 99%
“…С другой стороны, профиль скорости на срезе сопла, например, круглой микроструи при диаметре выходного отверстия сопла d ≤ 1 мм и удлинении канала сопла l/d ≥ 100 практически всегда будет иметь параболический характер ее распределения. Все особенности структуры и характеристик развития круглой и плоской микроструй в зависимости от изменений начальных условий на срезе сопла и акустического воздей-ствия представлены в работах [8][9][10][11][12][13]. Воздействие поперечного акустического поля на круглую микрострую приводит к ее уплощению, она становится квазиплоской и подвержена синусоидальной неустойчивости, как классическая плоская струя [11].…”
Section: Introductionunclassified
“…Воздействие поперечного акустического поля на круглую микрострую приводит к ее уплощению, она становится квазиплоской и подвержена синусоидальной неустойчивости, как классическая плоская струя [11]. Другой важной особенностью механизма развития как круглой, так и плоской микроструи является ее бифуркация (раздвоение) в поперечном акустическом поле [10][11][12][13]. Процесс раздвоения синусоидально неустойчивой микроструи приводит к возникновению двух разбегающихся под определенным углом струй, каждая из которых представляет собой набор когерентных вихревых структур.…”
Section: Introductionunclassified