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This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. This is the first time these powerful computational techniques have been published in book form.

Furthermore, certain "steady" flows are inherently unsteady in the presence of flow separation, as for example the unsteady flow caused by the Karman vortex shedding downstream of a cylin der and "static" airfoil stall which is an inherently unsteady flow phenomenon.

This book presents the solutions to the problems in convective heat transfer. It also contains computer programs to solve homework problems on the CD accompanying the book. These programs are based on differential and integral methods.

From the reviews: "The book has a broad and general coverage of both the mathematics and the numerical methods well suited for graduate students." Computer programs are also included for many problems together with a separate chapter dealing with the application of computer programs to heat transfer problems.