Titlebook: Global Stability Analysis of Shear Flows; Rameshkumar Bhoraniya,Gayathri Swaminathan,Vinod N Book 2023 The Editor(s) (if applicable) and T

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,Axisymmetric Boundary Layer on?a?Circular Cone,ered parallel to the axis of the cone at the inlet. The angle of attack is zero, and hence, the base flow is axisymmetric. The favourable pressure gradient develops in the streamwise direction due to the cone angle. The Reynolds number is calculated based on the cone radius (.) at the inlet and free

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,Boundary Layer on?an?Inclined Flat Plate,s. A symmetric wedge flow with different non-dimensional pressure gradient parameters (.) has been considered. The pressure gradient (.) in the flow direction is zero for ., favourable (negative) for . and adverse (positive) for .. The base flow is computed by the numerical solution of the Falkner-S

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https://doi.org/10.1007/978-3-322-86888-6ce the two commonly used approximations which result in a problem solvable locally at one streamwise location. These are the parallel flow assumption and the weakly non-parallel flow assumption. Some applications of each are described. Then we introduce strongly non-parallel flows and the global sta

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