【送料無料】 Theory of Publications Dover – Sections Wing 機械工学

Dover Publishing刊の Theory of Wing Sections: Including a Summary of Airfoil Data １冊です。4訂版 わかる内燃機関 廣安博之 わかる工学全書 日新出版 中古 03651F024。

古い本で、それなりの使用感はありますが、ページはきれいです。増補改訂自動車工学　 古書　昭和25年発行。

扉ページに、朱印（蔵書印？）を砂ゴムで消した跡があります。新・機械保全技能ハンドブック(油圧装置編)/日本プラントメンテナンス協会(編者)。（4枚目の写真）

それ以外は、書き込み、破れはありません。[A11704918]熱力学の基礎 第2版 I: 熱力学の基本構造 [単行本] 清水 明。

 

○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

 

○配送方法

 ゆうパケットポスト（発送用シール）（送料230円）で送ります。[送料無料]　’７９　全日本機械工具標準型録　カタログ　全機工連型録編集委員会　S54。

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