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Dover Books on Aeronautical Engineering Ser.: Aircraft Structures by David J. Peery and Engineering Careers Information Service Staff (2011, Trade Paperback)
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About this product
Product Identifiers
PublisherDover Publications, Incorporated
ISBN-100486485803
ISBN-139780486485805
eBay Product ID (ePID)104258810
Product Key Features
Number of Pages576 Pages
Publication NameAircraft Structures
LanguageEnglish
Publication Year2011
SubjectMechanics / Aerodynamics, Aeronautics & Astronautics
TypeTextbook
AuthorDavid J. Peery, Engineering Careers Information Service Staff
Subject AreaTechnology & Engineering, Science
SeriesDover Books on Aeronautical Engineering Ser.
FormatTrade Paperback
Dimensions
Item Weight28.9 Oz
Item Length9.2 in
Item Width6.1 in
Additional Product Features
Intended AudienceCollege Audience
LCCN2011-019335
Dewey Edition23
Dewey Decimal629.134/31
Table Of ContentPreface 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
SynopsisStill 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 NumberTL671.6.P4 2011
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