AERO ENG 484 - Analysis Of Laminated Composite Structures

Institution:
Missouri University of Science and Technology
Subject:
Aerospace Engineering
Description:
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. Prerequisite: Mech Eng 382 or Aero Eng 311. (Co-listed with Mech Eng 484)
Credits:
3.00
Credit Hours:
Prerequisites:
Corequisites:
Exclusions:
Level:
Instructional Type:
Lecture
Notes:
Additional Information:
Historical Version(s):
Institution Website:
Phone Number:
(573) 341-4111
Regional Accreditation:
North Central Association of Colleges and Schools
Calendar System:
Semester

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