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Theory of Wing Sections : Including a Summary of Airfoil Data.

By: Contributor(s): Material type: TextTextSeries: Dover Books on Aeronautical Engineering SeriesPublisher: Newburyport : Dover Publications, Incorporated, 1959Copyright date: �1959Edition: 1st edDescription: 1 online resource (677 pages)Content type:
  • text
Media type:
  • computer
Carrier type:
  • online resource
ISBN:
  • 9780486134994
Subject(s): Genre/Form: Additional physical formats: Print version:: Theory of Wing SectionsDDC classification:
  • 629.1/3432
LOC classification:
  • TL672 .A2
Online resources:
Contents:
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.
Summary: Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
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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.

Description based on publisher supplied metadata and other sources.

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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