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Victor Birman
Emeritus
Mechanical & Aerospace Engin
329 Coldstream Court
Rolla, MO 65409
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)
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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 |
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Attention Distance Students
For live class lectures, you will log in using the Zoom UM System link in Canvas. For accessing class recordings, you will need to contact your instructor directly.
| Enrollment Information | ||||
| Campus | Delivery Mode | Class Status | Class Nbr | Section |
| Distance Education | Online | OPEN | 70869 | 102 |
| Course Access Information | ||||
| Learning Management System | Canvas | |||