On the impulse response for swept boundary-layer flows

DOI10.1017/S0022112097006149zbMath0897.76026OpenAlexW2049322015WikidataQ61816661 ScholiaQ61816661MaRDI QIDQ4377309

R. J. Lingwood

Publication date: 9 February 1998

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112097006149

zbMATH Keywords

absolute instabilitylaminar-turbulent transitionpressure gradientflow anglechordwise directionthree-dimensional laminar boundary layers

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Parallel shear flows in hydrodynamic stability (76E05)

Related Items (6)

Attachment-line, cross-flow and Tollmien–Schlichting instabilities on swept ONERA-D and Joukowski airfoils ⋮ Absolute stability mechanism of a swept cylinder laminar boundary layer with imposed spanwise periodic conditions ⋮ Primary instability mechanisms on the magnetohydrodynamic boundary layer flow over a rotating disk subject to a uniform radial flow ⋮ Compressible Modes of the Rotating‐Disk Boundary‐Layer Flow Leading to Absolute Instability ⋮ Transition to turbulence in open flows: what linear and fully nonlinear local and global theories tell us ⋮ Identifying linear absolute instabilities from differential eigenvalue problems using sensitivity analysis

This page was built for publication: On the impulse response for swept boundary-layer flows