1986
DOI: 10.1017/s0022112086002227
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Numerical investigation of incompressible flow in grooved channels. Part 1. Stability and self-sustained oscillations

Abstract: Incompressible moderate-Reynolds-number flow in periodically grooved channels is investigated by direct numerical simulation using the spectral element method. For Reynolds numbers less than a critical value Rc the flow is found to approach a stable steady state, comprising an ‘outer’ channel flow, a shear layer at the groove lip, and a weak re-circulating vortex in the groove proper. The linear stability of this flow is then analysed, and it is found that the least stable modes closely resemble Tollmien–Schli… Show more

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Cited by 222 publications
(103 citation statements)
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“…The Reynolds numbers in our study based on the flow rate and the kinematic viscosity are 877 and 1271 on average and at the systolic peak, respectively. They are in good agreement with the critical Reynolds number for the onset of instability which is close to Re ¼ 975 (Ghaddar et al 1986). …”
Section: Discussionsupporting
confidence: 80%
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“…The Reynolds numbers in our study based on the flow rate and the kinematic viscosity are 877 and 1271 on average and at the systolic peak, respectively. They are in good agreement with the critical Reynolds number for the onset of instability which is close to Re ¼ 975 (Ghaddar et al 1986). …”
Section: Discussionsupporting
confidence: 80%
“…The reasons for the discrepancy seem to be the different flow conditions such as the much higher Reynolds number 1000-2000 of the flow in the aorta or the stenosed carotid. In the numerical study of flow over periodic grooves in a channel by Ghaddar et al (1986), the frequency of the selfsustained oscillation corresponding to the least unstable Tollmien -Schlichting mode was predicted from linear stability analysis. Our peak frequencies of patient C (around 24-58 Hz) seem to agree well with a frequency range (16 -24 Hz) found in their study; this frequency range corresponds to frequencies in grooves with non-dimensional separation distance L ¼ 5 and non-dimensional groove length l ¼ 2.5 with different depth (non-dimensionalized with the half-channel width).…”
Section: Discussionmentioning
confidence: 99%
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“…Such a n a p p r o a c h w as suggested by M a d a y, P atera, and R nquist 24] and analyzed by P erot 4] and Couzy 7] it follows classical splitting approaches (e.g., 18,26]) that lead to a Poisson equation for the pressure except that, in the present case, the splitting is e ected in the discrete form of the equations. The correct boundary conditions are preserved and no steady-state temporal errors are introduced.…”
Section: Stokes Operators To Complete the Description Of The Stokesmentioning
confidence: 87%
“…The ubiquity of fluid systems characterized by an n-periodic arrangement of identical units or by multi-periodic geometric features has spawned a great deal of analyses and simulations: flow in wavy or grooved channels [9,15,16,40] or past arrays of roughness elements and vortex generators [6], acoustics in periodic wave-guides [1], energy extraction from an buoy array [12] and, of course, flow in turbomachines [8,13,14,20,23,24,30] and combustors [5,28,29,31,38,39,45] are but a few examples that fall under this category. Not surprisingly, specific analysis and simulation techniques that efficiently address this periodicity have been developed, in particular for turbomachinery applications, typically describing blade-to-blade dynamics, aeroelastic properties, and rotor-stator interactions.…”
Section: Introductionmentioning
confidence: 99%