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Download PDF Theory of Wing Sections - Including a Summary of Airfoil Data

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Published by Dover Publishers. About this Item: Dover Publishers. Brand New. New edition. Language: English. Brand new Book. 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 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.

Seller Inventory AAC Seller Inventory BTE Condition: Fine. No Jacket.

Published by Unknown About this Item: Unknown, Ships with Tracking Number! May not contain Access Codes or Supplements. May be ex-library. Buy with confidence, excellent customer service!. Published by Dover Pubns About this Item: Dover Pubns, Paper Back. Condition: very Good. About this Item: Paperback. A reference for engineers and students, this volume devotes more than pages to theoretical and experimental considerations. It progresses from elementary materials to methods used in t. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.

It progresses from elementary materials to meth. Paperback or Softback. Seller Inventory BBS Published by Dover Publications About this Item: Dover Publications, Soft Cover. Condition: Very Good. Pages: ; Weight: 1lb 9. Cover has minor rubbing and edgewear, 2 faint creases on front cover, small sticker damage on the spine, otherwise clean, unmarked, tight.

Published by Dover Publications, NY Later Printing. Remainder mark on bottom edge. A nice, crisp copy. This book is in good condition only; study or reading copy only. The book has some shelfwear, light cover creasing, noticeable edge chipping to wraps. Inside pages have no writing. Unattractive but functional copy. Seller Inventory 08GW Seller Inventory mon From: Ground Zero Books, Ltd. Silver Spring, MD, U. Trade paperback. Reprint edition.

Cover has some creasing, wear and soiling. Minor ink marks and notes inside rear cover. This Dover edition, first published in is an unabridged and corrected republication of the first edition first published in by McGraw-Hill Book Company.


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This Dover edition includes a new Preface by the authors. The new edition reflected a continuing demand for a concise compilation of the subsonic aerodynamic characteristics of modern NACA wing sections together with a description of their geometry and associated theory. These wing sections, or their derivations, continued to be the most commonly used ones for airplanes designed for both subsonic and supersonic speeds, and for applicaitons to helicopter rotor blades, propeller blades, and high performance fans.

Ira Abbott - Wikipedia

Since original publication many new contributions had been made to the understanding of the boundary layer, the methods of boundary-layer control, and the effects of compressibility at super-critical speeds. These were acknowledged but not fully addressed in this revision. Ira H. Abbott July 18, - November 3, was an American aerospace engineer.

Abbott supervised the X, supersonic transport, nuclear rocket and advanced reentry programs. He retired in Methods and data are presented for using wing section 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. Seller Inventory q. Seller Inventory n. Condition: Used: Good. Condition: Brand New.

In Stock. Seller Inventory x Item added to your basket View basket. Learn how to enable JavaScript on your browser. NOOK Book. 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 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 Forces on Wings. Effect of Aspect Ratio. Application of Section Data to Monoplane Wings: a. Basic Concepts of Lifting-line Theory. Solutions for Linear Lift Curves.

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Generalized Solution. Applicability of Section Data. Concept of a Perfect Fluid. Equations of Motion. Description of Flow Patterns. Simple Two-dimensional Flows: a. Uniform Stream. Sources and Sinks. Circular Cylinder in a Uniform Stream. Circular Cylinder with Circulation.

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. Basic Concepts. Angle of Zero Lift and Pitching Moment. Design of Mean Lines. Engineering Applications of Section Theory. 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. Thickness Distributions.

Theory of Wing Sections: Including a Summary of Airfoil Data

Mean Lines. Numbering System. Approximate Theoretical Characteristics. Special Combinations of Thickness and Camber. Standard Aerodynamic Characteristics.


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Lift Characteristics: a. Angle of Zero Lift. Lift-curve Slope. Maximum Lift. Effect of Surface Condition on Lift Characteristics. Drag Characteristics: a. Minimum Drag of Smooth Wing Sections. Variation of Profile Drag with Lift Coefficient. Effect of Surface Irregularities on Drag Characteristics. Unconservative Wing Sections. Pitching moment Characteristics. Plain Flaps. Split Flaps. Slotted Flaps: a. Description of Slotted Flaps. Single-slotted Flaps. External-aifoil Flaps. Double-slotted Flaps. Leading-edge High-lift Devices: a.

Theory of Wing Sections Including a Summary of Airfoil Data Dover Books on Aeronautical Engineering