Titlebook: Shear Flow in Surface-Oriented Coordinate; Ernst Heinrich Hirschel,Wilhelm Kordulla Book 1981 Friedr. Vieweg & Sohn Verlagsgesellschaft mb

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Higher-Order Boundary-Layer Equations,separately the influence of wall curvature itself and the wall-curvature gradient, an approach which was found to be necessary by KUX [ 1]. No attempt is being made to review the numerous sets of governing equations (including the modeling of turbulence), which appeared in literature, and the corresponding methods to solve them.

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Conditions of Compatibility at the Body Surface,onsidered for compressible flows. Consistent with the remainder of the book the compatibility conditions will be given for steady flows in terms of the surface metric tensor a. for locally monoclinic coordinates.

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Introduction,eneral in flows of aerodynamic interest. In high-Reynolds-number flow viscous effects are important only in the immediate neighbourhood of the surface of the body considered, i.e. within the boundary layer. If the boundary layer remains attached to the surface, the interaction with the external invi

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Boundary-Layer Parameters,propriate diagonal elements of the covariant metric tensor yields the physical coordinates of the shear stress tensor (see chapter 8). Here only the contributions relevant in zero- or first-order boundary-layer theory are given.

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Stagnation - Point Solution,ilable is not intended, only a few references are mentioned here [40,53,68]. HOWARTH [40]was one of the first to present results for a general three-dimensional stagnation point. He considers the incompressible flow at a nodal point of attachment. LIBBY [53] reports a solution for compressible bound

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Quasi-Two-Dimensional Boundary Layers,y. Accordingly, the three-dimensional stagnation-point flow, discussed in chapter 4, is called quasi-onedimensional because only one coordinate, that normal to the wall, appears in the governing equations (4.4), (4.7) and (4.9). Quasitwo-dimensional boundary-layers are present, for example, in plane

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