Low-speed aerodynamics is important in the design and operation of aircraft flying at low Mach number, and ground and marine vehicles. This 2001 book offers a modern treatment of the subject, both the theory of inviscid, incompressible, and irrotational aerodynamics and the computational techniques now available to solve complex problems. A unique feature of the text is that the computational approach (from a single vortex element to a three-dimensional panel formulation) is interwoven throughout. Thus, the reader can learn about classical methods of the past, while also learning how to use numerical methods to solve real-world aerodynamic problems. This second edition has a new chapter on the laminar boundary layer (emphasis on the viscous-inviscid coupling), the latest versions of computational techniques, and additional coverage of interaction problems. It includes a systematic treatment of two-dimensional panel methods and a detailed presentation of computational techniques for three-dimensional and unsteady flows. With extensive illustrations and examples, this book will be useful for senior and beginning graduate-level courses, as well as a helpful reference tool for practising engineers.

The book aims at explaining the fundamental principles of aerodynamics from an engineer’s point of view. Right from the beginning, it conveys a basic understanding of the behaviour of the real viscous fluid. Later, through appropriate approximations, the ideal inviscid fluid is introduced. It gives a clear exposition of the fundamentals of fluid dynamics, both viscous and inviscid, including the topic of boundary layer. The text provides introductory concepts of wind tunnel and measurements to give a balanced overview of the subject so that the students are exposed to experiments and laboratory practices at the outset. It emphasises the physics of various aspects of the fluid flow phenomenon so that the reader develops a ‘physical feel’ of the subject. This book is primarily intended for the undergraduate students of aeronautical engineering and aerospace engineering. KEY FEATURES • Use of a large number of flow visualisation photographs for illustration • Use of a large number of innovative diagrams • Adequate number of worked-out examples at the end of almost all the chapters • A set of exercise problems at the end of every chapter

"Low Speed Aerodynamics" delves into the fundamental principles and phenomena associated with the behavior of airflow around bodies at low speeds. This book covers essential topics such as boundary layer theory, drag, lift, and stall characteristics, emphasizing practical applications in aviation and automotive industries. Through a blend of theoretical insights and experimental results, it provides a comprehensive understanding of aerodynamic principles, enabling engineers and researchers to design efficient and effective airfoil shapes and vehicles. Ideal for students and professionals, this work serves as a vital resource in the study of aerodynamics.

Now reissued by Cambridge University Press, this sixth edition covers the fundamentals of aerodynamics using clear explanations and real-world examples. Aerodynamics concept boxes throughout showcase real-world applications, chapter objectives provide readers with a better understanding of the goal of each chapter and highlight the key 'take-home' concepts, and example problems aid understanding of how to apply core concepts. Coverage also includes the importance of aerodynamics to aircraft performance, applications of potential flow theory to aerodynamics, high-lift military airfoils, subsonic compressible transformations, and the distinguishing characteristics of hypersonic flow. Supported online by a solutions manual for instructors, MATLAB® files for example problems, and lecture slides for most chapters, this is an ideal textbook for undergraduates taking introductory courses in aerodynamics, and for graduates taking preparatory courses in aerodynamics before progressing to more advanced study.

This book covers the application of computational fluid dynamics from low-speed to high-speed flows, especially for use in aerospace applications.

A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.