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Engineering
Aerospace Engineering
Aircraft Design and Structures
1. Introduction to Aircraft Design and Structures
2. Aircraft Design Process
3. Fundamentals of Aircraft Structures
4. Aircraft Loads Analysis
5. Structural Analysis of Aircraft Components
6. Structural Dynamics and Aeroelasticity
7. Fatigue and Fracture Mechanics
8. Structural Testing and Certification
Fundamentals of Aircraft Structures
Basic Solid Mechanics
Stress and Strain Concepts
Normal Stress
Shear Stress
Strain Tensor
Principal Stresses
Material Properties
Elasticity
Plasticity
Stress-Strain Curves
Poisson's Ratio
Young's Modulus
Shear Modulus
Yield Strength
Ultimate Strength
Bending of Beams
Bending Moment
Shear Force Diagrams
Neutral Axis
Section Modulus
Torsion of Shafts
Torsional Shear Stress
Angle of Twist
Thin-Walled Tube Torsion
Buckling of Columns
Euler Buckling
Slenderness Ratio
Critical Load Calculation
Aircraft Materials
Metallic Materials
Aluminum Alloys
Properties and Applications
Corrosion Resistance
Steel Alloys
High-Strength Steels
Stainless Steels
Titanium Alloys
High-Temperature Applications
Weight Considerations
Composite Materials
Fiber Reinforcements
Carbon Fiber
Glass Fiber
Aramid Fiber
Matrix Materials
Epoxy Resins
Thermoplastic Matrices
Laminate Theory
Ply Orientation
Stacking Sequence
Sandwich Structures
Core Materials
Face Sheets
Material Selection Criteria
Strength-to-Weight Ratio
Stiffness-to-Weight Ratio
Fatigue Resistance
Corrosion Resistance
Cost Considerations
Manufacturability
Repairability
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2. Aircraft Design Process
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4. Aircraft Loads Analysis