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This book presents a new method of asymptotic analysis of boundary-layer problems, the Successive Complementary Expansion Method (SCEM). The second part is devoted to SCEM and its applications in fluid mechanics, including external and internal flows.
This book presents the basic principles and theoretical foundations of three-dimensional attached viscous flows as they apply to aircraft of all kinds. Includes estimated flow properties, coordinates for fuselages and wings, and sample problems with solutions.
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