COMPOSITE
A Course on Practical Stress Analysis of Composite Materials - Aircraft Structures
A Course on Practical Stress Analysis of Composite Materials - Aircraft Structures
Practical Stress Analysis of Composite Materials – Aircraft Structures is a calculation-focused engineering course that teaches how to analyze composite aircraft components under real structural loading conditions.
The course covers isotropic and orthotropic layered materials, Classical Laminate Theory (CLT), interlaminar stresses, micromechanics, prepreg and sandwich structures, joints, thermal loading, fatigue, and certification aspects of composite structures.
Emphasis is placed on hands-on stress analysis through detailed numerical exercises and supporting finite-element (FE) analyses rather than on purely theoretical material science. Learners work through realistic aerospace case studies, including monolithic and sandwich aircraft structures, to build practical, industry-relevant competence.
01. Strength and Failure Modes of Prepreg Sheets
00:06:1102. Properties and Strength of Prepregs
00:04:4103. Exercise-341
00:01:2104. Prepregs: Strength and Material Properties
00:04:1705. Failure Theories: Metals vs Composites
00:02:0806. Exercise-342
00:04:0107. Exercise-342A
00:02:1608. Exercise-343
00:03:2109. Exercise-344
00:02:3401. Stress Concentration in Composites – Part 1
00:03:5402. Stress Concentration in Composites – Part 2
00:04:2603. Exercise-361
00:02:3104. Exercise-362
00:01:2905. Exercise-362A
00:02:1006. Exercise-363_Part1
00:04:2507. Exercise-363_Part2
00:00:5808. Exercise-364
00:02:3409. Important Notes on the OHT and OHC
00:02:0001. Joints
00:06:2802. Mechanical Joints - Failure Modes
00:03:0503. Exercise-371
00:03:2404. Notes on Bearing, Bypass, and Fastener Load Distribution
00:05:1205. Failure Modes and Analysis of Composite Bolted Joints
00:01:2106. Adhesive/Bonded Joints
00:04:4207. Bonded Joints: Strength and Behavior
00:06:4008. Environment Impact on Adhesive Joints
00:02:4109. Exercise-372
00:01:2510. Hybrid Joints
00:04:4201. Introduction to Fatigue, Durability, and Damage Tolerance
00:02:1802. Fatigue in composites - Part1
00:04:2103. Fatigue in composites - Part2
00:04:5604. Damage Tolerance in composites
00:02:5305. Regulatory Requirement for damage tolerance
00:03:0206. Design approach for damage tolerance
00:04:5007. Computational aspects of damage tolerance
00:07:45
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Students
2
language
English
Duration
10h 52mLevel
intermediate
Expiry period
3 Months
Certificate
Yes
AeroSIFT
English
Certificate Course
2 Students
10h 52m
5 Courses
5 Reviews