Emeritus
Mechanical & Aerospace Engin
329 Coldstream Court
Rolla, MO 65409
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 Aero Eng 6284)
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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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 | 70870 | 102 |
Course Access Information | ||||
Learning Management System | Canvas |