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

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9780486605869: Theory of Wing Sections: Including a Summary of Airfoil Data (Dover Books on Aeronautical Engineering)

"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.

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Abbott, Ira H.
ISBN 10: 0486605868 ISBN 13: 9780486605869
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Descripción 1959. PAP. Estado de conservación: New. New Book. Shipped from US within 10 to 14 business days. Established seller since 2000. Nº de ref. de la librería V0-9780486605869

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Abbott, Ira H.
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Descripción Dover Publishers. Estado de conservación: New. Brand New. Nº de ref. de la librería 0486605868

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Ira H. Abbott, A. E. Von Doenhoff
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Descripción Dover Publications Inc., United States, 1960. Paperback. Estado de conservación: New. New edition. 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. Nº de ref. de la librería AA99780486605869

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Ira H. Abbott, A. E. Von Doenhoff
Editorial: Dover Publications Inc., United States (1959)
ISBN 10: 0486605868 ISBN 13: 9780486605869
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Descripción Dover Publications Inc., United States, 1959. Paperback. Estado de conservación: New. New edition. 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. Nº de ref. de la librería AA99780486605869

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Descripción 1959. PAP. Estado de conservación: New. New Book.Shipped from US within 10 to 14 business days. Established seller since 2000. Nº de ref. de la librería IB-9780486605869

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Descripción Dover Publications. PAPERBACK. Estado de conservación: New. 0486605868 *BRAND NEW* Ships Same Day or Next!. Nº de ref. de la librería NATARAJB1FI1001390

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Descripción Dover Publications, 1959. Paperback. Estado de conservación: New. Nº de ref. de la librería 0486605868

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Descripción Dover Publications. PAPERBACK. Estado de conservación: New. 0486605868. Nº de ref. de la librería Z0486605868ZN

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Descripción Dover Publications, 1959. Estado de conservación: 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. . . . . . . Nº de ref. de la librería V9780486605869

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Descripción Dover Publications Inc. Paperback. Estado de conservación: new. BRAND NEW, Theory of Wing Sections (New edition), Ira H. Abbott, A. E. von Doenhoff. Nº de ref. de la librería B9780486605869

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