Postgraduate DiplomaAutomotive & Motorsport Applications open

Postgraduate Diploma in Cores, Sandwich and Critical Joints

Online 800-hour Postgraduate Diploma in Cores, Sandwich and Critical Joints. 8 modules covering ASTM C393 sandwich beam flexure, ASTM C297 flatwise tension of sandwich and Abaqus. Assigned tutor and open enrolment.

Duration800 h
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute diploma
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Learning outcomes

What you will be able to do

01

Select cores and facesheets for sandwich structures.

02

Calculate sandwich panels against their failure modes.

03

Manufacture sandwich panels with defect control.

04

Design adhesive joints with appropriate surface preparation.

05

Size mechanical and hybrid joints in composites.

06

Analyse critical safety joints in line with FIA requirements.

07

Plan validation tests for panels and joints.

Profile

Who it's for

  • Structures engineer who wants to specialise in Cores, Sandwich and Critical Joints.
  • Composite materials engineer who wants to specialise in Cores, Sandwich and Critical Joints.
  • FEM analysis engineer who wants to specialise in Cores, Sandwich and Critical Joints.
  • Composite manufacturing technician who wants to specialise in Cores, Sandwich and Critical Joints.
  • Test engineer who wants to specialise in Cores, Sandwich and Critical Joints.
  • Chassis design engineer who wants to specialise in Cores, Sandwich and Critical Joints.
  • Engineering or science graduates looking to enter motorsport competition.
Standards & tools

What you'll work with

  • ASTM C393 sandwich beam flexure
  • ASTM C297 flatwise tension of sandwich
  • ASTM C273 core shear
  • ASTM D5868 lap shear of reinforced plastics
  • ASTM D5961 bearing response
  • ASTM D7766 sandwich testing
  • CMH-17 Composite Materials Handbook
  • FIA Technical Regulations on safety structures
Syllabus

8 modules · 800 h

  1. 1.1Principle of sandwich structures
  2. 1.2Facesheets, core and adhesive
  3. 1.3Bending stiffness and mass efficiency
  4. 1.4Applications in chassis and bodywork
  5. 1.5Impact structures
  6. 1.6Advantages and limitations
  7. 1.7Selection of configurations
  8. 1.8Costs and manufacturability
  9. 1.9Examples of use in competition
  10. 1.10Workshop: comparison of panels by specific stiffness
  1. 2.1Aluminium honeycomb
  2. 2.2Nomex aramid honeycomb
  3. 2.3PMI and PVC foam cores
  4. 2.4Balsa and thermoplastic cores
  5. 2.5Density and cell size
  6. 2.6Shear and compression properties
  7. 2.7Temperature behaviour
  8. 2.8Moisture absorption
  9. 2.9Machining and shaping of the core
  10. 2.10Practical: core selection for a floor
  1. 3.1Sandwich beam theory
  2. 3.2Deflection from bending and shear
  3. 3.3Failure modes: facesheet buckling, wrinkling
  4. 3.4Core crushing
  5. 3.5Core shear failure
  6. 3.6Concentrated loads and inserts
  7. 3.7FEM analysis of panels
  8. 3.8Beam flexure tests
  9. 3.9Design with safety margins
  10. 3.10Laboratory: three-point bending test of a sandwich panel
  1. 4.1Co-curing versus secondary bonding
  2. 4.2Film adhesives and their curing
  3. 4.3Core stabilisation
  4. 4.4Vacuum and pressure control
  5. 4.5Defects: debonding and cell collapse
  6. 4.6Core ramps and edges
  7. 4.7Embedded inserts in the core
  8. 4.8Panel inspection
  9. 4.9Core repair
  10. 4.10Practical: manufacture of a panel with a Nomex core
  1. 5.1Adhesion theory
  2. 5.2Epoxy, acrylic and methacrylate adhesives
  3. 5.3Surface preparation by sanding and peel ply
  4. 5.4Joint geometries
  5. 5.5Stress distribution and peel
  6. 5.6Lap shear testing
  7. 5.7Ageing and environment
  8. 5.8Adhesive bond line control
  9. 5.9Defects and their detection
  10. 5.10Case study: adhesive bonding of a wing bracket
  1. 6.1Bolted joints in composites
  2. 6.2Failure modes: bearing, tear-out, tension
  3. 6.3Inserts and bushings
  4. 6.4Torque values and relaxation
  5. 6.5Riveted joints in composite panels
  6. 6.6Hybrid adhesive-mechanical joints
  7. 6.7Galvanic corrosion with carbon
  8. 6.8Metal-to-composite joints
  9. 6.9Joint fatigue
  10. 6.10Laboratory: bearing test of a drilled hole
  1. 7.1Suspension anchorages to the chassis
  2. 7.2Monocoque joints with impact structures
  3. 7.3Harness and seat anchorages
  4. 7.4Halo joints
  5. 7.5FIA static test requirements
  6. 7.6Periodic joint inspection
  7. 7.7Joint failure analysis
  8. 7.8Safety factors
  9. 7.9Calculation documentation
  10. 7.10Case study: analysis of a suspension anchorage
  1. 8.1Selection of the sandwich component
  2. 8.2Definition of loads
  3. 8.3Selection of core and facesheets
  4. 8.4Panel sizing
  5. 8.5Design of joints and inserts
  6. 8.6Finite element analysis
  7. 8.7Validation test plan
  8. 8.8Manufacturing plan
  9. 8.9Report and presentation
  10. 8.10Final review with the tutor
Methodology, software & labs

How you'll learn

100% online training on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. No fixed timetable: students progress at their own pace within the intake, which makes it possible to combine with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is Abaqus, Altair HyperWorks and OptiStruct, ESAComp, Ansys Mechanical, in free, academic or evaluation versions. Tests are studied using real test procedures for sandwich panel flexure, adhesive joint validation and suspension anchorage analysis. Assessment is continuous by module, plus the final integrating project.

Accreditable laboratories(EN ISO/IEC 17025) with rotor test rig, EMC/Lightning pre-compliance, HIL/SIL, vibration/acoustics.
Evidence-oriented final project:safety case, test plan, compliance dossier and operational limits.
Industry mentoring:instructors with experience in training, , eVTOL/UAM and flight test.
Flexible format(hybrid/online), international cohorts and support from SEIUM Career Services.
Ethics and safety:a safety-by-design approach, with cyber-OT, DIH and compliance as core pillars.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Selection of the sandwich component

Select cores and facesheets for sandwich structures.

Definition of loads

Calculate sandwich panels against their failure modes.

Selection of core and facesheets

Manufacture sandwich panels with defect control.

Panel sizing

Design adhesive joints with appropriate surface preparation.

Design of joints and inserts

Size mechanical and hybrid joints in composites.

Career opportunities

Where this takes you

Structures EngineerComposite Materials EngineerFEM Analysis EngineerComposite Manufacturing TechnicianTest EngineerChassis Design Engineer
Admissions & scholarships

Requirements

  • Prior technical training or professional experience in the sector. No university degree is required.
  • Internet connection and a computer capable of running the programme's software.
  • Sufficient Spanish to follow technical standards documentation.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

FAQ

Frequently asked questions

The programme totals 800 hours spread over 6 to 8 months. That is an average of 10 to 15 hours per week, compatible with full-time work.

The programme uses Abaqus, Altair HyperWorks and OptiStruct, ESAComp, Ansys Mechanical. Free, academic or evaluation versions are used, and the tutor indicates the free alternative where one exists.

SEIUM's own diploma upon passing the continuous assessment and the integrating project. It is an in-house programme, not an official qualification from the Ministry.

Yes. Modules passed in a course or diploma in the same area are recognised in the advanced programme. Check the recognition policy when you enrol.

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