Theory of Wing Sections

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9780486605869: Theory of Wing Sections

A reference for engineers and students, this volume devotes more than 300 pages to theoretical and experimental considerations. It progresses from elementary materials to methods used in the design of NACA low-drag airfoils, and it presents techniques for using wing-section data to predict wing characteristics. Requires differential and integral calculus and elementary mechanics. 1949 edition.

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PREFACE TO DOVER EDITION PREFACE 1. THE SIGNIFICANCE OF WING-SECTION CHARACTERISTICS Symbols. The Forces on Wings. Effect of Aspect Ratio. Application of Section Data to Monoplane Wings: a. Basic Concepts of Lifting-line Theory. b. Solutions for Linear Lift Curves. c. Generalized Solution. Applicability of Section Data. 2. SIMPLE TWO-DIMENSIONAL FLOWS Symbols. Introduction. Concept of a Perfect Fluid. Equations of Motion. Description of Flow Patterns. Simple Two-dimensional Flows: a. Uniform Stream. b. Sources and Sinks. c. Doublets. d. Circular Cylinder in a Uniform Stream. e. Vortex. f. Circular Cylinder with Circulation. 3. THEORY OF WING SECTIONS OF FINITE THICKNESS Symbols. Introduction. Complex Variables. Conformal Transformations. Transformation of a Circle into a Wing Section. Flow about Arbitrary Wing Sections. Empirical Modification of the Theory. Design of Wing Sections. 4. THEORY OF THIN WING SECTIONS Symbols. Basic Concepts. Angle of Zero Lift and Pitching Moment. Design of Mean Lines. Engineering Applications of Section Theory. 5. THE EFFECTS OF VISCOSITY Symbols. Concept of Reynolds Number and Boundary Layer. Flow around Wing Sections. Characteristics of the Laminar Layer. Laminar Skin Friction. Momentum Relation. Laminar Separation. Turbulent Flow in Pipes. Turburlent Skin Friction. Calculation of Thickness of the Turbulent Layer. Turbulent Separation. Transition from Laminar to Turbulent Flow. Calculation of Profile Drag. Effect of Mach Number on Skin Friction. 6. FAMILIES OF WING SECTIONS Symbols. Introduction. Method of Combining Mean Lines and Thickness Distributions. NACA Four-digit Wing Sections: a. Thickness Distributions. b. Mean Lines. c. Numbering System. d. Approximate Theoretical Characteristics. NACA Five-digit Wing Sections: a. Thickness Distributions. b. Mean Lines. c. Numbering System. d. Approximate Theoretical Characteristics. Modified NACA Four-and Five-digit Series Wing Sections. NACA 1-Series Wing Sections: a. Thickness Distributions. b. Mean Lines. c. Numbering System. d. Approximate Theoretical Characteristics. NACA 6-Series Wing Sections: a. Thickness Distributions. b. Mean Lines. c. Numbering System. d. Approximate Theoretical Characteristics. NACA 7-Series Wing Sections. Special Combinations of Thickness and Camber. 7. EXPERIMENTAL CHARACTERISTICS OF WING SECTIONS. Symbols. Introduction. Standard Aerodynamic Characteristics. Lift Characteristics: a. Angle of Zero Lift. b. Lift-curve Slope. c. Maximum Lift. d. Effect of Surface Condition on Lift Characteristics. Drag Characteristics: a. Minimum Drag of Smooth Wing Sections. b. Variation of Profile Drag with Lift Coefficient. c. Effect of Surface Irregularities on Drag Characteristics. d. Unconservative Wing Sections. Pitching moment Characteristics. 8. HIGH-LIFT DEVICES Symbols. Introduction. Plain Flaps. Split Flaps. Slotted Flaps: a. Description of Slotted Flaps. b. Single-slotted Flaps. c. External-aifoil Flaps. d. Double-slotted Flaps. Leading-edge High-lift Devices: a. Slats. b. Slots. c. Leading-edge Flaps. Boundary-layer Control. The Chordwise Load Distribution over Flapped Wing Sections. 9. EFFECTS OF COMPRESSIBILITY AT SUBSONIC SPEEDS Symbols. Introduction. Steady Flow through a Stream Tube: a. Adiabatic Law b. Velocity of Sound c. Bernoulli's Equation for Compressible Flow. d. Cross-sectional Areas and Pressures in a Stream Tube. e. Relations for a Normal Shock. First-order Compressibility Effects: a. Glauert-Prandtl Rule b. Effect of Mach Number on the Pressure Coefficient. Flow about Wing Sections at High Speed: a. Flow at Subcritical Mach Numbers. b. Flow at Supercritical Mach Numbers. Experimental Wing Characteristics at High Speeds: a. Lift Characteristics. b. Drag Characteristics. c. Moment Characteristics. Wings for High-speed Applications. REFERENCES APPENDIX I. Basic Thickness Forms II. Mean Lines III. Airfoil Ordinates IV. Aerodynamic Characteristics of Wing Sections INDEX

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Book by Abbott Ira H

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Abbott, Ira H.
ISBN 10: 0486605868 ISBN 13: 9780486605869
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Descrizione libro 1959. PAP. Condizione libro: New. New Book. Shipped from US within 10 to 14 business days. Established seller since 2000. Codice libro della libreria V0-9780486605869

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Descrizione libro Dover Publications Inc., United States, 1960. Paperback. Condizione libro: New. New edition. 214 x 149 mm. Language: English . Brand New Book. 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. Codice libro della libreria AA99780486605869

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Ira H. Abbott, A. E. Von Doenhoff
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Descrizione libro Dover Publications Inc., United States, 1960. Paperback. Condizione libro: New. New edition. 214 x 149 mm. Language: English . Brand New Book. 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. Codice libro della libreria AA99780486605869

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Descrizione libro 1959. PAP. Condizione libro: New. New Book.Shipped from US within 10 to 14 business days. Established seller since 2000. Codice libro della libreria IB-9780486605869

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Descrizione libro Dover Publications, 1959. Paperback. Condizione libro: New. Codice libro della libreria 0486605868

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Descrizione libro Dover Publications Inc. Paperback. Condizione libro: new. BRAND NEW, Theory of Wing Sections (New edition), Ira H. Abbott, A. E. von Doenhoff. Codice libro della libreria B9780486605869

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Ira H. Abbott, A. E. von Doenhoff
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ISBN 10: 0486605868 ISBN 13: 9780486605869
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Descrizione libro Dover Publications, 1959. Condizione libro: New. 1959. Paperback. Series: Dover Books on Aeronautical Engineering. Num Pages: 703 pages, 350pp tables. BIC Classification: TGMF1; TRP. Category: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly; (UU) Undergraduate; (XV) Technical / Manuals. Dimension: 211 x 147 x 36. Weight in Grams: 814. 703 pages, 350pp tables. Cateogry: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly; (UU) Undergraduate; (XV) Technical / Manuals. BIC Classification: TGMF1; TRP. Dimension: 211 x 147 x 36. Weight: 732. . . . . . . Codice libro della libreria V9780486605869

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Ira H. Abbott, A. E. von Doenhoff
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Descrizione libro Dover Publications. Condizione libro: New. 1959. Paperback. Series: Dover Books on Aeronautical Engineering. Num Pages: 703 pages, 350pp tables. BIC Classification: TGMF1; TRP. Category: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly; (UU) Undergraduate; (XV) Technical / Manuals. Dimension: 211 x 147 x 36. Weight in Grams: 814. 703 pages, 350pp tables. Cateogry: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly; (UU) Undergraduate; (XV) Technical / Manuals. BIC Classification: TGMF1; TRP. Dimension: 211 x 147 x 36. Weight: 732. . . . . . Books ship from the US and Ireland. Codice libro della libreria V9780486605869

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Ira H. Abbott
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Descrizione libro Dover Publications. Paperback. Condizione libro: New. Paperback. 693 pages. Dimensions: 8.3in. x 5.7in. x 1.4in.Most useful in working with wing sections and methods for using section data to predict wing characteristics . . . much detailed geometric and aerodynamic data. Mechanical EngineeringThe 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 NACAs 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. This item ships from multiple locations. Your book may arrive from Roseburg,OR, La Vergne,TN. Paperback. Codice libro della libreria 9780486605869

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