1. SECOND CYCLE - MASTER'S DEGREE
  2. THE GRADUATE SCHOOL OF NATURAL AND APPLIED SCIENCES
  3. MECHANICAL ENGINEERING DEPARTMENT
  4. 1111 Mechanical Engineering
Course Information Course Learning Outcomes Course's Contribution To Program ECTS Workload Course Details
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COURSE INFORMATION
Course CodeCourse TitleL+P HourSemesterECTS
MAK 552THEORY OF COMPOSITE PLATES AND SHELLS3 + 02nd Semester7,5

COURSE DESCRIPTION
Course Level Master's Degree
Course Type Elective
Course Objective Klasik tabaka teorisi kullanılarak kompozit plak ve kabukların analizini öğrenme
Course Content Introduction to Analysis of Laminates, Theory of Laminated Plates, Theory of Laminated Plates with Coupling, Stiffness Characteristics of Selected Laminate Configurations, Symmetric and Antisymmetric Laminates, Quasi-Isotropic Laminates, Derivation and Use of Laminate, Inversions of Laminate Force-Deformation Equation, Determination of Lamina Stresses and Strains, Determination of Laminate Engineering Constants, Hygrothermal Effects in Laminates, Hygrothermal Degradation of Laminates, Hygrothermal Stresses in Laminates, Laminate Hygrothermal Expansion Coefficient, Interlaminar Stresses, Laminate Strength Analysis, First Ply Failure due to In-Plane Stresses, Delamination due to Interlaminar Stresses, Deflection and Buckling of Laminates, Analysis of Small Transverse Deflections, Buckling Analyzing, Selection of Laminate Design, Analysis of Plates Composed of Composite Materials, Anisotropic Plates Utilizing Classical Plate Theory, Anisotropic Plates Including Transverse Shear Deformation, Reissner’s Variational Theorem and Its Applications, Behavior of Simply-Supported, Cross-Ply Laminated Plates under Static Lateral and Plane Loads, The Elastic Stability of Specially Orthotropic Plates Due To In-Plane Loads For Various Boundary Conditions, Anisotropic Shells Utilizing Classical Shell Theory, Anisotropic Shells Including Transverse Shear Deformation, Anisotropic Laminated Cylindrical Shells, Stress in a Circular Cylindrical Shell Subjected To a Localized Load.
Prerequisites No the prerequisite of lesson.
Corequisite No the corequisite of lesson.
Mode of Delivery Face to Face

COURSE LEARNING OUTCOMES
1Learning analysis of composite plates and shells by using CLT.

COURSE'S CONTRIBUTION TO PROGRAM
PO 01PO 02PO 03PO 04PO 05PO 06PO 07PO 08PO 09PO 10PO 11PO 12PO 13PO 14
LO 00155443443534544
Sub Total55443443534544
Contribution55443443534544

ECTS ALLOCATED BASED ON STUDENT WORKLOAD BY THE COURSE DESCRIPTION
ActivitiesQuantityDuration (Hour)Total Work Load (Hour)
Course Duration (14 weeks/theoric+practical)14342
Hours for off-the-classroom study (Pre-study, practice)14570
Assignments14040
Final examination14343
Total Work Load

ECTS Credit of the Course





195

7,5
COURSE DETAILS
 Select Year   


 Course TermNoInstructors
Details 2015-2016 Spring1MUZAFFER TOPÇU
Details 2011-2012 Spring1HASAN ÇALLIOĞLU


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Course Details
Course Code Course Title L+P Hour Course Code Language Of Instruction Course Semester
MAK 552 THEORY OF COMPOSITE PLATES AND SHELLS 3 + 0 1 Turkish 2015-2016 Spring
Course Coordinator  E-Mail  Phone Number  Course Location Attendance
MUH A02129 %
Goals Klasik tabaka teorisi kullanılarak kompozit plak ve kabukların analizini öğrenme
Content Introduction to Analysis of Laminates, Theory of Laminated Plates, Theory of Laminated Plates with Coupling, Stiffness Characteristics of Selected Laminate Configurations, Symmetric and Antisymmetric Laminates, Quasi-Isotropic Laminates, Derivation and Use of Laminate, Inversions of Laminate Force-Deformation Equation, Determination of Lamina Stresses and Strains, Determination of Laminate Engineering Constants, Hygrothermal Effects in Laminates, Hygrothermal Degradation of Laminates, Hygrothermal Stresses in Laminates, Laminate Hygrothermal Expansion Coefficient, Interlaminar Stresses, Laminate Strength Analysis, First Ply Failure due to In-Plane Stresses, Delamination due to Interlaminar Stresses, Deflection and Buckling of Laminates, Analysis of Small Transverse Deflections, Buckling Analyzing, Selection of Laminate Design, Analysis of Plates Composed of Composite Materials, Anisotropic Plates Utilizing Classical Plate Theory, Anisotropic Plates Including Transverse Shear Deformation, Reissner’s Variational Theorem and Its Applications, Behavior of Simply-Supported, Cross-Ply Laminated Plates under Static Lateral and Plane Loads, The Elastic Stability of Specially Orthotropic Plates Due To In-Plane Loads For Various Boundary Conditions, Anisotropic Shells Utilizing Classical Shell Theory, Anisotropic Shells Including Transverse Shear Deformation, Anisotropic Laminated Cylindrical Shells, Stress in a Circular Cylindrical Shell Subjected To a Localized Load.
Topics
WeeksTopics
1 Equations of Anisotropic Elasticity,
2 Virtual Work Principles, and Variational Methods
3 Introduction to Composite Materials
4 The Classical Laminated Plate Theory
5 The First-Order Laminated Plate Theory
6 Laminate Stiffnesses for Selected Laminates
7 One-Dimensional Analysis of Laminated Composite Plates
8 Analysis of Laminated Beams
9 exam
10 Cylindrical Bending
11 Vibration Suppression in Beams
12 Analysis of Specially Orthotropic Laminates
13 Bending of Rectangular Plates with Various Boundary Conditions
14 Theory and Analysis of Laminated Shells
Materials
Materials are not specified.
Resources
Course Assessment
Assesment MethodsPercentage (%)Assesment Methods Title
Final Exam50Final Exam
Midterm Exam50Midterm Exam
L+P: Lecture and Practice
PQ: Program Learning Outcomes
LO: Course Learning Outcomes