Theory of Wing Sections : Including a Summary of Airfoil Data.
Material type:
- text
- computer
- online resource
- 9780486134994
- 629.1/3432
- TL672 .A2
Intro -- Title Page -- Copyright Page -- PREFACE TO DOVER EDITION -- PREFACE -- Table of Contents -- CHAPTER 1 - THE SIGNIFICANCE OF WING-SECTION CHARACTERISTICS -- 1.1. Symbols. -- 1.2. The Forces on Wings. -- 1.3. Effect of Aspect Ratio. -- 1.4. Application of Section Data to Monoplane Wings. -- 1.5. Applicability of Section Data. -- CHAPTER 2 - SIMPLE TWO-DIMENSIONAL FLOWS -- 2.1. Symbols. -- 2.2. Introduction. -- 2.3. Concept of a Perfect Fluid. -- 2.4. Equations of Motion. -- 2.5. Description of Flow Patterns. -- 2.6. Simple Two-dimensional Flows. -- CHAPTER 3 - THEORY OF WING SECTIONS OF FINITE THICKNESS -- 3.1. Symbols. -- 3.2. Introduction. -- 3.3. Complex Variables. -- 3.4. Conformal Transformations. -- 3.5. Transformation of a Circle into a Wing Section. -- 3.6. Flow about Arbitrary Wing Sections. -- CHAPTER 4 - THEORY OF THIN WING SECTIONS -- 4.1. Symbols. -- CHAPTER 5 - THE EFFECTS OF VISCOSITY -- 5.1. Symbols. -- 5.2. Concept of Reynolds Number and Boundary Layer. -- 5.6. Momentum Relation. -- CHAPTER 6 - FAMILIES OF WING SECTIONS -- 6.1. Symbols. -- CHAPTER 7 - EXPERIMENTAL CHARACTERISTICS OF WING SECTIONS -- 7.1. Symbols. -- 7.2. Introduction. -- CHAPTER 8 - HIGH-LIFT DEVICES -- 8.1. Symbols. -- 8.2. Introduction. -- 8.3. Plain Flaps. -- CHAPTER 9 - EFFECTS OF COMPRESSIBILITY AT SUBSONIC SPEEDS -- REFERENCES -- APPENDIXES -- INDEX.
Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
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Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
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