Dover Publishing刊の Theory of Wing Sections: Including a Summary of Airfoil Data １冊です。
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○内容
"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.
出版社 ： Dover Publications, Inc. New York
著者 ： Ira H. Abbott and Albert. E. von Doenhoff
刊行日 ： 1959
言語 ： 英語
ペーパーバック ： 704ページ
寸法・重さ ： 21 x 14 x 3.5cm、 770g
ISBN ： 0486605868
○目次 （5枚目の写真）
CONTENTS
PREFACE TO DOVER EDITION............ v
PREFACE............................. vii
1. THE SIGNIFICANCE OF WING-SECTION CHARACTERISTICS .... 1
2. SIMPLE TWO-DIMENSIONAL FLOWS............... 31
3. THEORY OF WING SECTIONS OF FINITE THICKNESS ...... 46
4.THEORY OF THIN WING SECTIONS ............. 64
5.THE EFFECTS OF VISCOSITY.............. 80
6. FAMILIES OF WING SECTIONS............... 111
7. EXPERIMENTAL CHARACTERISTICS OF WING SECTIONS .... 124
8. HIGH-LIFT DEVICES ........ 188
9. EFFECTS OF COMPRESSIBILITY AT SUBSONIC SPEEDS ..... 247
REFERENCES...................... 300
APPENDIX
I. Basic Thickness Forms.... 309
II. Mean Lines ....... 382
III. Airfoil Ordinates.... 406
IV. Aerodynamic Chnracteristies of Wing Sections.... 449
INDEX ...................... 689
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