An Engineering Approach To The Calculation Of Aerodynamic Flows
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An Engineering Approach to the Calculation of Aerodynamic Flows
This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. The contents include two-dimensional and three-dimensional steady and unsteady flows with and without compressibility effects. The former theory is based on the numerical solutions of the reduced Navier-Stokes equations in which Euler and boundary-layer equations are coupled with an interaction law. The latter theory is based on the linear stability theory and employs the so-called e(n) method. The book details applications of this approach to airfoils, wings and high lift systems. It is intended for undergraduate and graduate students and practicing engineers interested in aerodynamics, hydrodynamics and modern numerical methods and computer programs for solving linear and nonlinear ordinary and parabolic partial differential equations.
An Engineering Approach to the Calculation of Aerodynamic Flows
This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. The contents include two-dimensional and three-dimensional steady and unsteady flows with and without compressibility effects. The former theory is based on the numerical solutions of the reduced Navier-Stokes equations in which Euler and boundary-layer equations are coupled with an interaction law. The latter theory is based on the linear stability theory and employs the so-called e(n) method. The book details applications of this approach to airfoils, wings and high lift systems. It is intended for undergraduate and graduate students and practicing engineers interested in aerodynamics, hydrodynamics and modern numerical methods and computer programs for solving linear and nonlinear ordinary and parabolic partial differential equations.
Aerodynamics for Engineering Students
Aerodynamics for Engineering Students, Fifth Edition, is the leading course text on aerodynamics. The book has been revised to include the latest developments in flow control and boundary layers, and their influence on modern wing design as well as introducing recent advances in the understanding of fundamental fluid dynamics. Computational methods have been expanded and updated to reflect the modern approaches to aerodynamic design and research in the aeronautical industry and elsewhere, and the structure of the text has been developed to reflect current course requirements. The book is designed to be accessible and practical. Theory is developed logically within each chapter with notation, symbols and units well defined throughout, and the text is fully illustrated with worked examples and exercises. The book recognizes the extensive use of computational techniques in contemporary aeronautical design. However, it can be used as a stand-alone text, reflecting the needs of many courses in the field for a thorough grounding in the underlying principles of the subject. The book is an ideal resource for undergraduate and postgraduate students in aeronautical engineering. The classic text, expanded and updated.Includes latest developments in flow control, boundary layers and fluid dynamics.Fully illustrated throughout with illustrations, worked examples and exercises.