Course I: Aircraft Composite Structures: Mechanics & Materials
Course Outline
- 1. Introduction and Composite Fundamentals
- 1.1 Types of Composites; Why composites; History of applications
- 1.2 Nano, Micro and Macro behavior of composites
- 1.3 Anisotropic and tailored-made properties
- 1.4 Fundamental reinforcing mechanisms
- 1.5 Key differences between composites and metals
- 2. Properties of Fiber, Matrix and Composite
- 2.1 Functions of fiber, matrix and interface
- 2.2 Typical properties of fiber, matrix and composite
- 2.3 Raw material forms
- 2.4 Manufacturing of CFRP prepreg
- 2.5 Engineering properties of prepreg
- 3. Tooling and Manufacturing Processes
- 3.1 Layup tooling types and material selection
- 3.2 Thermal growth and other key issues in tool design
- 3.3 Bond assembly jigs and secondary tooling
- 3.4 Hand layup, Bag molding, compression molding
- 3.5 Pultrusion, FW, RTM, VaRTM, CAPRI, RTL
- 3.6 Manufacturing defects and quality control
- 3.7 Skill check problems
- 4. Composite Fabrication Practice
- 4.1 Bagging materials, hand layup and curing process
- 4.2 Hands-on laminate fabrication by group at Intec
- 4.3 Tour of composite manufacturing and testing facilities
- 4.4 Coupon testing; comparison of lab results with theory
- 5. Micromechanics
- 5.1 Elastic constants and Poisson's ratio
- 5.2 Fiber and matrix stresses near a broken fiber
- 5.3 Tensile strength of unidirectional composites
- 5.4 Micro buckling of fibers in compression
- 5.5 Examples; Skill check problems
- 6. Review of Liner Elasticity
- 6.1 Stress, strain, equilibrium equations, compatibility
- 6.2 Transformation of stress and strain tensors
- 6.3 Constitutive equations for linearly elastic materials
- 6.4 2-D plane stress and plane strain problems
- 6.5 Examples; Skill check problems
- 7. Stress-Strain Relations of a Lamina
- 7.1 2-D stress-strain relations along the material axes
- 7.2 Determination of orthotropic material constants
- 7.3 2-D stress-strain relation along the reference axes
- 7.4 Apparent modulus of an off-axis lamina
- 7.5 Examples; Skill check problems
- 8. Classical Lamination Theory
- 8.1 In-plane forces, bending and twisting moments
- 8.2 Derivation of classical lamination theory
- 8.3 Shear coupling in unbalanced laminates
- 8.4 Bending and stretching of unsymmetric laminates
- 8.5 Examples; Skill check problems
- 9. Hygrothermal Behavior
- 9.1 Heat conduction and moisture diffusion
- 9.2 Hygrothermal stress-strain relations for a lamina
- 9.3 General CLT with hygrothermal effects
- 9.4 Hygrothermal effects on material properties
- 9.5 Examples; Skill check problems
- 10. Failure Criteria for Orthotropic Materials
- 10.1 Maximum stress/strain criteria
- 10.2 Tsai-Hill criterion
- 10.3 Tsai-Wu criterion
- 10.4 Other criteria
- 10.5 Examples; Skill check problems
- 11. Stiffness and Strength Analyses of a Laminate
- 11.1 Apparent laminate stiffness; Carpet plots
- 11.2 Laminate strength analysis procedure
- 11.3 Failure envelopes; Examples
- 11.4 Progressive failure analysis
- 11.5 Examples; Skill check problems
- 12. Free-Edge Interlaminar Effects
- 12.1 Free-body diagrams of free edge stresses
- 12.2 Analysis of free edge interlaminar stresses
- 12.3 Effects of stacking sequence
- 12.4 Design guidelines
- 12.5 Examples; Skill check problems
- 13. Bending and Buckling of Laminated Plates
- 13.1 Governing equations and boundary conditions
- 13.2 Solutions for specially orthotropic laminates
- 13.3 Effects of anisotropy and boundary conditions
- 13.4 Effects of plate geometry on buckling loads
- 13.5 Examples; Skill check problems
- 14. Fracture of Notched Composites
- 14.1 Fracture mechanics for metals
- 14.2 Hole size effects in composites
- 14.3 WEK, WN, and Mar-Lin fracture models
- 14.4 Examples of Notched strength prediction
- 14.5 Examples; Skill check problems
- 15. Structural Testing
- 15.1 Mechanical property tests
- 15.2 Test standards and specimen configurations
- 15.3 Data reduction procedures
- 15.4 Element and component tests
- 15.5 Skill check problems
- 16. Inspection and Repair
- 16.1 Typical in-service and manufacturing damages
- 16.2 NDI methods and probability of detection
- 16.3 Typical bolted and bonded repairs
- 16.4 Critical issues in composite repair
- 16.5 Skill check problems
Texts
Jones, R. M., Mechanics of Composite Materials, 2nd Edition,
Taylor & Francis, Philadelphia, PA, 1999 (Textbook); ISBN: 1-56032-712-X.
(Required)
Click here to order through Amazon.com
or BarnesandNoble.com.
László P. Kollár, and George S. Springer, Mechanics of Composite Structures, Cambridge University press, 2003, ISBN 0521801656
Niu, Michael, Composite Airframe Structures, Conmilit Press, 1992, ISBN 962-7128-06-6.
Gibson, R. F., Principles of Composite Materials Mechanics, McGraw-Hill, 1994
Hoskin, B. C., and Baker, A. A. (Ed.), Composite Materials for Aircraft Structures, AIAA Educational Series, New York, NY, 1986
Instructor
Dr. Kuen Lin
is a Professor in the Department of Aeronautics and Astronautics at the University of Washington. He is a Co-Director of the FAA Center of Excellence for Advanced Materials at UW. Dr. Lin obtained his Masters and Ph.D. degrees in the field of Aeronautical Structures and Composite Materials from Massachusetts Institute of Technology. Dr. Lin has over 30 years of research and development experience in advanced composite materials and structures. In addition to his research endeavors, Dr. Lin has concentrated his teaching on the subjects of mechanics of composite materials, foundation of solid mechanics, and finite element methods.Questions
If you have questions about this program, please call UW Educational Outreach Advising at 206-685-8936 in the greater Seattle area or 1-800-543-2320. If you have questions about registration for this program, please call the UW Educational Outreach Registration Department at 206-543-2310 or 1-800-543-2320.
For more information about Boeing initiatives in composites education, email Michael Richey, Boeing Learning Training and Development, Engineering & Operations Group.