Graduate Certificate in Composite Materials
This online graduate certificate program is designed for engineering and science professionals who are new to the field of composite materials or wish to expand their knowledge of composite materials.
MEEG616—Composite Materials Structures, taught by Dr. Jack R. Vinson, provides an introduction to composite materials; anisotropic elasticity and laminate theory; plates and panels of composite materials; beams, columns and rods; composite material shell structures; energy methods; strength and failure theories; adhesive bonding and mechanical fastening; hygrothermal effects; stress analysis, buckling, vibrations and impact.
MEEG617 – Composite Materials, taught by Dr. Erik Thostenson, discusses fiber and matrix materials; fiber-matrix interface; polymer, metal, ceramic and carbon matrix composites; geometric aspects, elastic properties, lamination theory, strength of unidirectional composites, strength of laminates, durability, hybrid composites, flexible composites and textile structural composites. ONLINE.
MEEG655 – Principles of Composites Manufacturing (3 credits), taught by Dr. Suresh G. Advani, introduces the fundamental principles involved in composites manufacturing. Modeling of such processes is emphasized with applications of injection molding, compression molding, filament wiring, pultrusion and resin transfer molding. ONLINE.
MEEG811–Sandwich Structures (3 credits), taught by Dr. Jack R. Vinson, studies composite and isotropic sandwich structures for stresses, deformations, buckling loads, natural frequencies and dynamic response under mechanical and environmental loads, involving honeycomb, solid, foam, web and truss core sandwich comprising beam, plate, ring and shell structures. Design and minimum weight optimization are treated.
MEEG818–Plates and Shells in Aerospace Structures I (3 credits), taught by Dr. Jack R. Vinson, examines the theory of plates from three-dimensional equations of elasticity. Small deflection analysis of rectangular and circular plates; thermoelastic effects; analysis of orthotropic plates, multilayered plates and sandwich panels; Green’s functions; energy methods; Reissner variational theorem for plates of moderate thickness; and large deflections of plates are other topics discussed. This course requires background obtained from MEEG610 (Intermediate Solid Mechanics), MEEG813 (Theory of Elasticity), or an equivalent course.
MEEG819–Plates and Shells in Aerospace Structures II (3 credits)* Dr. Jack R. Vinson covers the general theory of thin shells from three-dimensional equations of elasticity; shells of revolution under axially symmetric loads; asymmetric loads; thermoelastic effects; general bending theory, membrane theory, inextensional theory; Donnell equations; edge load solutions; orthotropic shells; laminated shells. This course requires background obtained from MEEG610 (Intermediate Solid Mechanics), MEEG813 (Theory of Elasticity), or an equivalent course.
*MEEG818 is not a prerequisite to this course.