Optimal Disturbances in Boundary Layers Subject to Streamwise Pressure Gradient
Author(s) -
Anatoli Tumin,
David E. Ashpis
Publication year - 2003
Publication title -
aiaa journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.828
H-Index - 158
eISSN - 1081-0102
pISSN - 0001-1452
DOI - 10.2514/2.6825
Subject(s) - adverse pressure gradient , pressure gradient , mechanics , boundary layer , subject (documents) , flow separation , boundary (topology) , geology , physics , aerospace engineering , mathematics , mathematical analysis , computer science , engineering , library science
Laminar-turbulent transition in shear flows is still an enigma in the area of fluid mechanics. The conventional explanation of the phenomenon is based on the instability of the shear flow with respect to infinitesimal disturbances. The conventional hydrodynamic stability theory deals with the analysis of normal modes that might be unstable. The latter circumstance is accompanied by an exponential growth of the disturbances that might lead to laminar-turbulent transition. Nevertheless, in many cases, the transition scenario bypasses the exponential growth stage associated with the normal modes. This type of transition is called bypass transition. An understanding of the phenomenon has eluded us to this day. One possibility is that bypass transition is associated with so-called algebraic (non-modal)
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