Separated Flows and Jets 1991
DOI: 10.1007/978-3-642-84447-8_73
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Research on Laminar Separation Bubbles at Delft University of Technology

Abstract: SI.l!l'ID'illY'!his paper gives a review of research at Delft Uni versi ty of Technology on laminar separation b.Il±>les. Results of flow visualisation studies are used to define an empirical relation for the angle ~ at which the se~ation streamline leaves the wall. The "e-to-the-n" transition predictIon method is extended to separated flows. A universal description of the laminar part of the b.Il±>le is proposed, resulting in a simple b.Il±>le prediction method.

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Cited by 15 publications
(24 citation statements)
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“…These results are consistent with results from other systems where sintered targets were compared to solidified targets [18]. The basic explanation is related to the relative density of the targets.…”
Section: 4supporting
confidence: 91%
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“…These results are consistent with results from other systems where sintered targets were compared to solidified targets [18]. The basic explanation is related to the relative density of the targets.…”
Section: 4supporting
confidence: 91%
“…The implication of this result is that if one uses a spectroscopic technique on the plume to determine composition of an unknown sample, there could be errors due to differential scattering in the plume and the limited detection angle [18]. However, we have shown that the particulates are not affected by such plume scattering and maintain the target composition.…”
Section: Discussionmentioning
confidence: 76%
“…From the famous Schubauer and Skramstad 31 experiment (Fig. 5) [14] it follows that at low turbulence levels a transition region is found that extends from Re x = 2.8 x 10…”
Section: Some Useful Relations From Boundary Layer Theorymentioning
confidence: 92%
“…If we calculate n as a function of x for a range of frequencies we get a set of n-curves; the envelope of these curves gives the maximum amplification factor N which occurs at any x. Figure 4 [14] shows as an example the nfactor calculation for the flat plate without suction using the new database. From the famous Schubauer and Skramstad 31 experiment (Fig.…”
Section: Some Useful Relations From Boundary Layer Theorymentioning
confidence: 99%
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