Stability and Transition in Shear Flows. By P. J. SCHMID & D. S. HENNINGSON. Springer, 2001. 556 pp. ISBN 0-387-98985-4. £ 59.50 or $79.95
By Peter J. Schmid, Dan S. Henningson. Journal of Fluid Mechanics, 2000
1,581 citations recorded by the source corpus.
Subfields: Computational Mechanics, Earth-Surface Processes
View Paper: https://www.semanticscholar.org/paper/c82f472e4add43a2b6429fc61d2b6d33bf80d105
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Citations in the corpus
- The large-scale dynamics of near-wall turbulence (2002, methodology): “Active or passive streaks In a linearized approximation, the equations for ωy and φ are the Squire and Orr– Sommerfeld equations of stability theory (Schmid & Henningson 2001), and their relation is hierarchical.”
- A critical-layer framework for turbulent pipe flow (2010, background): “The scaling of the width of these regions can be determined by consideration of the appropriate terms in (4.5) (for plane flow see Maslowe 1981; Schmid & Henningson 2001; Drazin & Reid 2004).”
- Algebraic growth in a Blasius boundary layer: optimal and robust control by mean suction in the nonlinear regime (2004, background): “…is a mechanism which appears to reconcile the seeming contrast between classical stability theory (based on the growth or decay of a single-mode perturbation) and experimental observations of the initial phases of transition in boundary layers, channels and pipes (cf. Schmid & Henningson 2001).”
- Issues in active flow control: theory, control, simulation, and experiment (2004, background): “Transient growth has explained shortcomings of linear stability theory in classic one-dimensional basic flows [22], that illustrates the difficulties in relying upon linear stability analysis in any but the simpliest problems.”
- Transition in boundary layers subject to free-stream turbulence (2004, background): “It is now understood that since the linearized Navier–Stokes operator is non-normal for many flow cases, a significant transient growth may occur before the subsequent exponential behaviour (Butler & Farrell 1992; Reddy & Henningson 1993; Schmid & Henningson 2001).”
- Linearized pipe flow to Reynolds number 10 7 (2003, background): “Three classical incompressible shear flows have received attention in connection with the phenomenon of ‘‘subcritical’’ or ‘‘nonmodal’’ or ‘‘bypass’’ transition to turbulence [9,28].”
- Direct optimal growth analysis for timesteppers (2008, background): “an exponential function of time multiplying a fixed modal shape; therefore, eigenvalue problem (4) is simply not directly relevant [15, 16].”
- Amplification of coherent streaks in the turbulent Couette flow: an input–output analysis at low Reynolds number (2010, methodology): “…frequencies) and Farrell & Ioannou (1993b) and Jovanović & Bamieh (2005) for the optimal stochastic response of laminar channel flows (see also e.g. Schmid & Henningson 2001; Schmid 2007, for a review), and the results of del Álamo & Jiménez (2006) and Pujals et al. (2009) for the optimal…”
- Spectral proper orthogonal decomposition and its relationship to dynamic mode decomposition and resolvent analysis (2017, methodology): “It has been used to study the linear response of flows to external body forces and perturbations (Trefethen et al., 1993; Farrell & Ioannou, 2001; Schmid & Henningson, 2001; Jovanović & Bamieh, 2005; Bagheri et al., 2009; Sipp et al., 2010) and to forcing from the nonlinear terms in the…”
- Transition of streamwise streaks in zero-pressure-gradient boundary layers (2002, background): “…point of view, it is now clear that since the linearized Navier–Stokes operator is non-normal for many flow cases (e.g. shear flows), a significant transient growth may occur before the subsequent exponential behaviour (see Butler & Farrell 1992; Reddy & Henningson 1993; Schmid & Henningson 2001).”
- Linear feedback control and estimation of transition in plane channel flow (2003, background): “Several transition scenarios initiated by perturbations experiencing non-modal growth have been investigated; for a recent review of subcritical transition scenarios, see Schmid & Henningson (2001).”
- Numerical investigation of the tone noise mechanism over laminar airfoils (2007, methodology): “The numerical method used to solve the iNS equations in a perturbation form is based on a Chebyshev collocation method (for more details see Schmid & Henningson 2001).”