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Aircraft Structures [Dover Books on Aeronautical Engineering] by David J. Peery

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All net proceeds will support Goodwill Industries of San Diego County

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Item specifics

Condition
Good: A book that has been read but is in good condition. Very minimal damage to the cover including ...
ISBN
9780486485805

About this product

Product Identifiers

Publisher
Dover Publications, Incorporated
ISBN-10
0486485803
ISBN-13
9780486485805
eBay Product ID (ePID)
104258810

Product Key Features

Number of Pages
576 Pages
Publication Name
Aircraft Structures
Language
English
Publication Year
2011
Subject
Mechanics / Aerodynamics, Aeronautics & Astronautics
Type
Textbook
Author
David J. Peery, Engineering Careers Information Service Staff
Subject Area
Technology & Engineering, Science
Series
Dover Books on Aeronautical Engineering Ser.
Format
Trade Paperback

Dimensions

Item Weight
28.9 Oz
Item Length
9.2 in
Item Width
6.1 in

Additional Product Features

Intended Audience
College Audience
LCCN
2011-019335
Dewey Edition
23
Dewey Decimal
629.134/31
Table Of Content
Preface 1. Equlibrium of Forces 2. Space Structures 3. Inertia Forces and Load Factors 4. Moments of Inertia, Mohr's Circle 5. Shear and Bending-Moment Diagrams 6. Shear and bending Stresses in Symmetrical Beamsd 7. Beams with Unsymmetrical Cross Sections 8. Analysis of Typical Members of Semimonocoque Structures 9. Spanwise Air-Load Distribution. 10. External Loads om the Airplane 11. Mechanical Properties of Aircraft Materials 12. Joints and Fittings 13. Design of Members in Tension, Bending, or Torison 14. Design of Compression Members 15. Design of Webs in Shear 16. Deflections of Structures 17. Statistically Indertiminate Structures 18. Special Methods of Analysis Appendix Index
Synopsis
Still relevant decades after its 1950 publication, this legendary reference text on aircraft stress analysis is considered the best book on the subject. It emphasizes basic structural theory, which remains unchanged with the development of new materials and construction methods, and the application of the elementary principles of mechanics to the analysis of aircraft structures. Suitable for undergraduate students, this volume covers equilibrium of forces, space structures, inertia forces and load factors, shear and bending stresses, and beams with unsymmetrical cross sections. Additional topics include spanwise air-load distribution, external loads on the airplane, joints and fittings, deflections of structures, and special methods of analysis. Topics involving a knowledge of aerodynamics appear in final chapters, allowing students to study the prerequisite aerodynamics topics in concurrent courses., This legendary, still-relevant reference text on aircraft stress analysis discusses basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition.
LC Classification Number
TL671.6.P4 2011

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