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Aero Eng 6284: Analysis of Laminated Composite Structures
An overview of isotropic beams, plates, and shells. Bending, vibration, and buckling of laminated composite beams and plates: exact and approximate solutions. Development of composite shell theory and simplified solutions. Analysis of composite structures including transverse shear deformation and thermal effects.(Co-listed with Mech Eng 6284)
Additional Info:
AeroEng/MechEng 6284-Course Announcement
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Time/Day: 04:00 pm - 06:30 pm W Prerequisites: Mech Eng 5282 or Aero Eng 5282. Units: 3 Course Component(s): Lecture Introduction Video: Intro |
Group Project: no Live Participation Required: no Download Restrictions: allowed upon request |
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Books: no textbook required |
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| Enrollment Information | ||||
| Campus | Delivery Mode | Class Status | Class Nbr | Section |
| Distance Education | Internet | OPEN | 71378 | 1DIS |
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| Learning Management System | Canvas | |||