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Structures d'avions [Livres de Douvres sur le génie aéronautique] par David J. Peery
9,32 $US
Environ12,85 $C
État :
Bon
Un livre qui a été lu, mais qui est en bon état. La couverture présente des dommages infimes, par exemple des éraflures, mais aucun trou ni aucune déchirure. Dans le cas des livres à reliure, la jaquette peut ne pas être incluse. La reliure présente des traces d'usure minimes. La plupart des pages ne sont pas endommagées et les plis, les déchirures, les passages soulignés ou surlignés et les inscriptions en marge sont minimes. Il n'y a aucune page manquante.
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Expédition :
Sans frais USPS Media MailTM.
Lieu : San Diego, California, États-Unis
Livraison :
Livraison prévue entre le mer. 6 août et le ven. 8 août à 94104
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Numéro de l'objet eBay :156637092465
Dernière mise à jour : août 03, 2025 06:39:31 HAEAfficher toutes les modificationsAfficher toutes les modifications
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Caractéristiques de l'objet
- État
- ISBN
- 9780486485805
À propos de ce produit
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
Language
English
Publication Name
Aircraft Structures
Subject
Mechanics / Aerodynamics, Aeronautics & Astronautics
Publication Year
2011
Type
Textbook
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
Description de l'objet du vendeur
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