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Astronomy & Space Science - Theory of Wing Sections: Including a Summary of Airfoil Data (Dover Books on Aeronautical Engineering)

Description

Book Synopsis: "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.

Details

Looking to enhance your knowledge of aeronautical engineering? Look no further than the Theory of Wing Sections: Including a Summary of Airfoil Data book. This comprehensive guide provides a concise compilation of the subsonic aerodynamics characteristics of modern NASA wing sections, making it an invaluable resource for engineers and students. With over 300 pages dedicated to both theoretical and experimental considerations, this book covers everything from elementary concepts to the design of NACA low-drag airfoils. Whether you're working with wing sections or predicting wing characteristics, this book has all the data you need for accurate analysis.

With its detailed geometric and aerodynamic data, the Theory of Wing Sections book is a must-have for those working in the field of aeronautical engineering. As the ones most commonly used for airplanes, helicopter rotor blades, propeller blades, and high-performance fans, the included wing sections and their derivatives are essential for anyone involved in designing aircrafts for subsonic and supersonic speeds. Plus, with judiciously selected plots and cross-plots of experimental data, you can easily correlate and simplify your analyses, saving you time and effort.

Mathematics knowledge may be necessary, but the Theory of Wing Sections book has been designed to minimize complex mathematical concepts. Assuming the reader has a basic understanding of differential and integral calculus, as well as elementary mechanics, this book focuses on providing practical and applicable information to help you in your engineering endeavors. The appendix alone contains over 350 pages of invaluable tables, including Basic Thickness Forms, Mean Lines, Airfoil Ordinates, and Aerodynamic Characteristics of Wing Sections.

Don't miss out on this incredible resource for aeronautical engineers and students. Take your knowledge to new heights with the Theory of Wing Sections book. Order your copy today and gain access to a wealth of essential information that will undoubtedly enhance your understanding of wing sections and their characteristics.

Click here to order the Theory of Wing Sections book now.

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