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Aerospace Structures
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Eric Raymond Johnson, Virginia Tech
Copyright Year:
Publisher: Virginia Tech Publishing
Language: English
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Attribution-NonCommercial-ShareAlike
CC BY-NC-SA
Table of Contents
1. Function of Flight Vehicle Structural Members
2. Aircraft Loads
3. Elements of Thin-Walled Bar Theory
4. Some Aspects of the Structural Analysis
5. Work and Energy Methods
6. Applications of Castigliano's Theorems
7. Arches, Rings, and Fuselage Frames
8. Laminated Bars of Fiber-Reinforced Polymer Composites
9. Failure Initiation in FRP Compositives
10. Structural Stability of Discrete Conservative Systems
11. Buckling of Columns and Plates
12. Introduction to Aeroelasticity
13. Fracture of Cracked Members
14. Design of a Landing Strut and Wing Spar
15. Direct Stiffness Method
16. Applications of the Direct Stiffness Method
17. Finite Element Method
18. Introduction to Flexible Body Dynamics
Appendix A: Linear Elasticity of Solid Bodies
Ancillary Material
Submit ancillary resourceAbout the Book
Aerospace Structures by Eric Raymond Johnson is a 600+ page text and reference book for junior, senior, and graduate-level aerospace engineering students. The text begins with a discussion of the aerodynamic and inertia loads acting on aircraft in symmetric flight and presents a linear theory for the status and dynamic response of thin-walled straight bars with closed and open cross-sections. Isotropic and fiber-reinforced polymer (FRP) composite materials including temperature effects are modeled with Hooke’s law. Methods of analyses are by differential equations, Castigliano’s theorems, the direct stiffness method, the finite element method, and Lagrange’s equations. There are numerous examples for the response axial bars, beams, coplanar trusses, coplanar frames, and coplanar curved bars. Failure initiation by the von Mises yield criterion, buckling, wing divergence, fracture, and by Puck’s criterion for FRP composites are presented in the examples.
Professors, if you are considering or reviewing this book for adoption in your course, please let us know here.
Problem sets: http://hdl.handle.net/10919/104169
ePub and LaTeX source files: Expected late spring 2022
About the Contributors
Author
Eric Raymond Johnson is emeritus professor of aerospace and ocean engineering at Virginia Tech. He earned his doctoral degree in applied mechanics from the University of Michigan in 1976, and from 1976 to 2003 was a member of the engineering faculty at Virginia Tech. Dr. Johnson s research area is composite structures. Research activities include the mechanics of the response and failure of advanced composite material structures with applications to flight and land vehicles, buckling and post-buckling of plates and shells, progressive failure analysis for the prediction of energy absorption in laminated composites and in bonded joints, and fracture mechanics. He has sixty-four publications in structural mechanics, and has been awarded research funding from government agencies and industries.. He is a senior member of the American Institute of Aeronautics and Astronautics and a member of the American Society of Mechanical Engineers.