1992
DOI: 10.1017/s0022112092002507
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The forced turbulent wall jet

Abstract: The effects of external two-dimensional excitation on the plane turbulent wall jet were investigated experimentally and theoretically. Measurements of the streamwise component of velocity were made throughout the flow field for a variety of imposed frequencies and amplitudes. The present data were always compared to the results generated in the absence of external excitation. Two methods of forcing were used: one global, imposed on the entire jet by pressure fluctuations in the settling chamber and one local, … Show more

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Cited by 48 publications
(19 citation statements)
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“…The theoretical results of this computing program were confirmed with good approximation with the Olson results and with the results obtained by more recent studies made by Katz (1992) [12 ] and other researchers.…”
Section: The Bistable Fluidic Power Element Using the Coanda Effectsupporting
confidence: 86%
“…The theoretical results of this computing program were confirmed with good approximation with the Olson results and with the results obtained by more recent studies made by Katz (1992) [12 ] and other researchers.…”
Section: The Bistable Fluidic Power Element Using the Coanda Effectsupporting
confidence: 86%
“…A key feature is the developing shear layer and the recirculation region above. The turbulent shear flow is somehow analogous to a wall jet although basic differences between ideal wall jet and hydraulic jumps include the effect of longitudinal pressure gradient P/x < 0, conservation of mass, and the natural forcing which is likely to enhance the two-dimensionality and periodicity of coherent structures (Katz et al, 1992). In the jump, the maximum velocity V max decays longitudinally as x -1/2 (Chanson and Brattberg 2000, Murzyn and Chanson 2009, Chanson 2010c.…”
Section: Hydraulic Jumpsmentioning
confidence: 99%
“…The results presented in [4], however, indicate that the unsteady coherent motion strongly influences the mean flow of the turbulent wall jet. In addition, if the coherent motion is a result of a local flow instability, then steady turbulent simulations are unlikely to capture the relevant physics correctly Therefore, in order to understand these physical mechanisms, an unsteady simulation spanning many eddy turnover times of the large coherent motion is necessary; at the same time, the simulation has to be accurate enough to account for the random turbulent motion.…”
Section: Introductionmentioning
confidence: 82%
“…4 For case 1 (Figure 22a) which has the lowest Reynolds number, Re N = 75, the flow spreads rapidly after exiting the nozzle and separates after a short distance of about 60° from the nozzle. In this case, the jet is not energetic enough to remain attached for very long.…”
Section: Dns Of Coanda Flowsmentioning
confidence: 99%
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