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Instructor: Birman, Victor
Email: vbirman@mst.edu

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:

Aero/MechEng 6284-Syllabus


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
Books:

No textbook required.


Attention Distance Students

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For other course content: please contact your instructor.

Enrollment Information
Campus Delivery Mode Class Status Class Nbr Section
Distance Education Internet OPEN 75850 1DIS

Course Access Information
Learning Management System Canvas