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:
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, distance are not required to attend synchronous lectures. Download Restrictions: Must request permission from instructor. |
Books: The course is based on a variety of research papers, books and reports. No single textbook can cover the material we study. One of the textbooks that may particularly useful is: R.F. Gibson, "Principles of Composite Material Mechanics," Fourth edition, CRC Press, Taylor & Francis Group, Boca Raton, Florida, 2016. |
Attention Distance Students
For classes produced by I.T. MediaServices: Access to live and archived media will be available in MediaSpace at mst.mediaspace.kaltura.com or in Panopto at mst.hosted.panopto.com. For more information email itms@mst.edu.
For other course content: please contact your instructor.
Enrollment Information | ||||
Campus | Delivery Mode | Class Status | Class Nbr | Section |
Distance Education | Internet | OPEN | 71255 | 102 |
Course Access Information | ||||
Learning Management System | Canvas |