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High Speed Wing Theory

✍ Scribed by Doris Cohen; Robert Thomas Jones


Publisher
Princeton University Press
Year
2015
Tongue
English
Leaves
250
Series
Princeton Aeronautical Paperbacks; 2204
Category
Library

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✦ Synopsis


Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes.

Originally published in 1960.

The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

✦ Table of Contents


Preface
Contents
A. Aerodynamics of Wings at High Speeds
Chapter 1. Fundamental Considerations in the Development of Wings for High Speeds
1. Review of Wing Theory for Low Speeds
2. Incompressible Flow in Two Dimensions. The Theory of Thin Airfoils
3. Effects of Compressibility at Subsonic Speeds
4. Effect of Sweepback
Chapter 2. Aerodynamics of Thin Wings at Subsonic Speeds
5. Extension of Thin Airfoil Theory to Three Dimensions
6. Lifting Surfaces
7. Lifting Surfaces. Solutions for Specified Planforms
8. Lifting Surfaces of Slender Planform
9. Thickness Distributions
Chapter 3. Aerodynamics of Thin Wings at Supersonic Speeds
10. Fundamental Considerations
11. Two-Dimensional Flow
12. The Drag of Lifting Surfaces in Three-Dimensional Flow
13. Determination of Lift in Three-Dimensional Flow. Methods and Formulas
14. Specific Planforms. Lift Distribution, Lift and Drag Due to Angle of Attack
15. Wave Drag and Pressure Distribution Due to Thickness
16. Cited References and Bibliography


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