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S & T Global - St. Louis
Engineering Education Ctr (MS&T)
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)
Time/Day: 04:00 pm - 06:30 pm W
Prerequisites: Mech Eng 5282 or Aero Eng 5282.
Course Component(s): Lecture
Group Project: no
Live Participation Required: no
Download Restrictions: allowed upon request
no textbook required
Attention Distance Students
For EdTech Media produced classes: Access to live and archived media is thru MediaSpace.
For other course content: please contact your instructor.
|Campus||Delivery Mode||Class Status||Class Nbr||Section|
|Missouri S&T Global St. Louis||Face-to-Face||OPEN||71212||1S|
|Course Access Information|
|Learning Management System||Canvas|