Theory of Wing Sections
Product ID: 280102965
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"Most useful in working with wing sections and methods for using section data to predict wing characteristics . . . much detailed geometric and aerodynamic data." -- Mechanical Engineering The first edition of this work has been corrected and republished in answer to the continuing demand for a concise compilation of the subsonic aerodynamics characteristics of modern NASA wing sections together with a description of their geometry and associated theory. These wing sections, or their derivatives, continue to be the ones most commonly used for airplanes designed for both subsonic and supersonic speeds, and for helicopter rotor blades, propeller blades, and high performance fans. Intended to be primarily a reference work for engineers and students, the book devotes over 300 pages to theoretical and experimental considerations. The theoretical treatment progresses from elementary considerations to methods used for the design of NACA low-drag airfoils. Methods and data are presented for using wingsection data to predict wing characteristics, and judiciously selected plots and cross-plots of experimental data are presented for readily useful correlation of certain simplifying assumptions made in the analyses. The chapters on theory of thin wings and airfoils are particularly valuable, as is the complete summary of the NACA's experimental observations and system of constructing families of airfoils. Mathematics has been kept to a minimum, but it is assumed that the reader has a knowledge of differential and integral calculus, and elementary mechanics. The appendix of over 350 pages contains these tables: Basic Thickness Forms, Mean Lines, Airfoil Ordinates, and Aerodynamic Characteristics of Wing Sections. Review: Genial - Era para un regalo y el receptor dice que es genial Review: RAS - Le livre était difficile à trouver par le canal des libraires, dommage
| Best Sellers Rank | #277,569 in Books ( See Top 100 in Books ) #481 in Aerospace Engineering #1,453 in Astronomy & Space Science #2,105 in Transportation |
| Customer Reviews | 4.7 out of 5 stars 231 Reviews |
E**A
Genial
Era para un regalo y el receptor dice que es genial
S**N
RAS
Le livre était difficile à trouver par le canal des libraires, dommage
L**O
The best book
Abbot is one of the scholars guys that encourages other people to be like him, I think the complex theories about potential flow, finite span airfoil and wing, and many experimental data about almost a complete family of NACA series are the main focus of this book, I appreciate all those professors that made this field my passion
R**.
Perfetto
Libro chiaro e completo, un must nel settore
R**U
Essential reference, cuts through fundamentals, lots of wing data
First, someone highly recommended this text. I am not disappointed. In two parts, this book has a math beginning and abundant graphical summary of airfoil performance. Starting with Wing-Section characteristics, the forces on airfoils and their response to those forces are covered in 2D, 3D then fluid analysis. Symbols used in each chapter are identified prior to use. Theoretical treatment is a progression of the developing insight in symbolic approximation from the contributors to understanding aerospace engineering. Many of the equations are represented in graphs so one can grasp it quickly and then proceed with the math. Even then, the authors provide a quick precis for a perspective on defining solutions. Many times they seek the quick and simple, not simplistic, heads up approach while not flubbing on the math. So, while Theory of Wing Sections is not an introductory text, it is an excellent supplement or toolbox to deliver achievable options along with their performance and limitations. Many designers or engineers dig into the graphical data section to explore well tried airfoils as a prelude to computer firmware analysis which may not divulge the underlying methods a given design is based. This book takes the mystery out of the meat. To truly ferret through the fundamental concepts here, one should have a working knowledge of calculus prepared to use it. However, one can find use of this work studying the graphical wing section data noting the Reynold's numbers apply to full size aircraft. One starts here for UAV model scale aircraft, then digs deeper.
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