ISBN: 9780486605869 - theory of wing sections: including a summary of airfoil data (dover books on aeronautical engineering) (38 Ergebnisse)

Zustand: Good. Good condition. A copy that has been read but remains intact. May contain markings such as bookplates, stamps, limited notes and highlighting, or a few light stains.

Paperback. Zustand: Very Good. It's a well-cared-for item that has seen limited use. The item may show minor signs of wear. All the text is legible, with all pages included. It may have slight markings and/or highlighting.

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Paperback. Zustand: Acceptable. Connecting readers with great books since 1972. Used textbooks may not include companion materials such as access codes, etc. May have condition issues including wear and notes/highlighting. We ship orders daily and Customer Service is our top priority.

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Paperback. Zustand: Fair. No Jacket. Readable copy. Pages may have considerable notes/highlighting. ~ ThriftBooks: Read More, Spend Less.

Paperback. Zustand: Fair. No Jacket. Readable copy. Pages may have considerable notes/highlighting. ~ ThriftBooks: Read More, Spend Less.

Trade Paperback. Zustand: Acceptable. Dover edition, first published in 1959. This trade paperback is in fair condition. The cover shows significant wear, including creases and scuff marks, and the spine has noticeable wear along the edges. The interior pages are clean, though the cover bears a previous owner's name. No dust jacket is present, as typical for this format. unknown (no dust jacket present).…

Zustand: very_good. Gently read. May have name of previous ownership, or ex-library edition. Binding tight; spine straight and smooth, with no creasing; covers clean and crisp. Minimal signs of handling or shelving. 100% GUARANTEE! Shipped with delivery confirmation, if you're not satisfied with purchase please return item! Ships USPS Media Mail.…

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Zustand: New. Brand New.

Paperback. Zustand: Very Good. The book has been read, but is in excellent condition. Pages are intact and not marred by notes or highlighting. The spine remains undamaged.

Hardcover. Zustand: Like New. First Edition. First Edition, First Printing. Published by Dover Publications, 1959. Octavo. Hardcover. Book is like new. Dust jacket is like new.

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PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000.

Paperback. Zustand: new. Paperback. Reference for engineers and students progresses from elementary materials to methods used in design of NACA low-drag airfoils. Presents techniques for using wing-section data to predict wing characteristics. "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. Reference for engineers and students progresses from elementary materials to methods used in design of NACA low-drag airfoils. Presents techniques for using wing-section data to predict wing characteristics. 1949 edition. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.…

Paperback. Zustand: New. 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.…

Paperback. Zustand: Brand New. new dover edition edition. 693 pages. 8.25x5.75x1.25 inches. In Stock.

Trade paperback. Zustand: Good. Reprint edition. x,693, [1] pages. Illustrations. Formulae. Index. Cover has some creasing, wear and soiling. Minor ink marks and notes inside rear cover. This Dover edition, first published in 1959 is an unabridged and corrected republication of the first edition first published in 1949 by McGraw-Hill Book Company. This Dover edition includes a new Preface by the authors. Dr. Abbott was the Director of Aeronautical and Space Research at NASA and Dr. von Doenhoff was a NASA research engineer. 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. 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, 1906 - November 3, 1988) was an American aerospace engineer. A graduate of MIT, Abbott worked for Langley Aeronautical Laboratory in 1929. He was a Director of Aeronautical and Space Research at NASA during the middle of the twentieth century and before that was employed by the National Advisory Committee for Aeronautics (NACA). Abbott supervised the X-15, supersonic transport, nuclear rocket and advanced reentry programs. He retired in 1962. As Assistant Director of NACA, Abbott was decisive in keeping Ames Research Center focused on research instead of moving into operations during the development of the proposed Orbiting Astronomical Observatory in 1960. In recognition for his "outstanding contributions" to airfoil research and his leadership, he was inducted into the first round of the NACA/NASA Hall of Fame on August 13, 2015. "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" 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 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. 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.…

Zustand: New. 1960. New edition. 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. . . . . . …

Zustand: New. pp. 703.

Zustand: New.

Zustand: New. In English.

Zustand: As New. Unread book in perfect condition.

Zustand: New. 1960. New edition. 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. …

Paperback. Zustand: Brand New. new dover edition edition. 693 pages. 8.25x5.75x1.25 inches. In Stock.

Paperback / softback. Zustand: New. New copy - Usually dispatched within 3 working days.

Zustand: New. pp. 703.