CourseAerospace, UAM, Drones & Space Applications open

Advanced propulsion refrigeration course

Online course of 300 hours in advanced cooling in propulsion: 6 modules covering the need for advanced cooling, internal blade cooling, film and effusion cooling, materials and coatings, cooling in electrified propulsion, and a propulsion cooling project, with an assigned technical tutor.

Duration300 hours · 3 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute certificate
Virtual lab · try it before you enrol

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Learning outcomes

What you will be able to do

01

Understand the thermal limits that drive advanced cooling in propulsion.

02

Design internal blade cooling channels.

03

Analyse film, effusion and transpiration cooling.

04

Select materials and thermal barrier coatings.

05

Size cooling systems for electrified propulsion.

06

Evaluate the performance cost of each cooling solution.

07

Design a cooling solution for a propulsion component.

Profile

Who it's for

  • Turbine cooling engineers.
  • Heat transfer engineers moving into propulsion.
  • Thermal CFD engineers working on hot-section components.
  • High-temperature materials engineers who need to understand cooling design.
  • Electric propulsion thermal management engineers.
  • Propulsion researchers.
  • Engineering or science graduates looking to join engine manufacturers.
Standards & tools

What you'll work with

  • EASA CS-E (certification specifications for engines)
  • 14 CFR Part 33 (airworthiness standards for aircraft engines)
  • ASTM C633 (adhesion or cohesion strength of thermal spray coatings)
  • ASTM E1461 (thermal diffusivity by the flash method)
  • ASME V&V 20-2009 (verification and validation in computational fluid dynamics and heat transfer)
  • SAE AS755F (aircraft propulsion system performance station designation)
  • Ansys CFX
  • STAR-CCM+
  • COMSOL Multiphysics
  • Ansys Mechanical
  • nTop
Syllabus

6 modules

  1. 1.1Gas temperatures above the material limit
  2. 1.2Cooling effectiveness and parameters
  3. 1.3Thermodynamic cost of cooling air
  4. 1.4Historical evolution of cooling techniques
  5. 1.5Requirements in electric and hybrid propulsion
  6. 1.6Cooling in rockets and ramjets
  7. 1.7Manufacturing constraints
  8. 1.8Metrics for comparing solutions
  9. 1.9Challenges in next-generation engines
  10. 1.10Case study: cooling across three generations of engines
  1. 2.1Serpentine channels with turbulators
  2. 2.2Pedestals and pin fins
  3. 2.3Jet impingement cooling
  4. 2.4Leading- and trailing-edge cooling
  5. 2.5Double-wall channels
  6. 2.6Rotation effects in channels
  7. 2.7Internal Nusselt correlations
  8. 2.8Pressure loss in internal passages
  9. 2.9Topology optimisation of channels
  10. 2.10Workshop: designing a serpentine channel with turbulators
  1. 3.1Mechanism of the cooling film
  2. 3.2Adiabatic film effectiveness
  3. 3.3Cylindrical and shaped holes
  4. 3.4Effusion in combustor liners
  5. 3.5Blowing and density ratios
  6. 3.6Interaction with the mainstream flow
  7. 3.7Porous transpiration cooling
  8. 3.8Tests with pressure-sensitive paint
  9. 3.9CFD simulation of film cooling
  10. 3.10Lab: film effectiveness with different geometries
  1. 4.1Nickel-based single-crystal superalloys
  2. 4.2Thermal barrier coatings
  3. 4.3Bond coats and oxidation
  4. 4.4Ceramic matrix composites
  5. 4.5CMAS degradation
  6. 4.6Adhesion and diffusivity testing
  7. 4.7Additive manufacturing of complex channels
  8. 4.8Non-destructive inspection of coatings
  9. 4.9Combining material and cooling
  10. 4.10Practical exercise: calculating the temperature drop across a thermal barrier
  1. 5.1Losses in electric motors and electronics
  2. 5.2Liquid cooling of inverters
  3. 5.3Cold plates and microchannels
  4. 5.4Phase change and heat pipes
  5. 5.5In-flight battery cooling
  6. 5.6Ram-air heat exchangers and their drag
  7. 5.7Using cryogenic fuel as a heat sink
  8. 5.8Cooled cooling air
  9. 5.9Integrated thermal loop architectures
  10. 5.10Case study: cooling a 500 kW electric motor
  1. 6.1Component and operating conditions
  2. 6.2Material temperature requirements
  3. 6.3Selection of cooling techniques
  4. 6.4Geometric design of the solution
  5. 6.5Thermal and fluid simulation
  6. 6.6Assessment of the performance cost
  7. 6.7Manufacturing feasibility
  8. 6.8Comparison of alternatives
  9. 6.9Report and presentation
  10. 6.10Final project: final review with the tutor
Methodology, software & labs

How you'll learn

A 100% online programme on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within each intake, so you can combine it with your job.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is Ansys CFX, STAR-CCM+, COMSOL Multiphysics, Ansys Mechanical and nTop, in free, academic or evaluation versions. Testing is studied through real procedures for designing internal cooling channels, simulating film cooling and sizing cooling systems for power electronics. Assessment is continuous by module, plus the final project.

Standards covered: EASA CS-E, 14 CFR Part 33, ASTM C633, ASTM E1461, ASME V&V 20-2009, SAE AS755F

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of EASA CS-E, 14 CFR Part 33, ASTM C633 and ASTM E1461 applied to real cases, not as a theoretical annex.
Industry software:Ansys CFX, STAR-CCM+, COMSOL Multiphysics, Ansys Mechanical, nTop, in free, academic or evaluation versions.
Final project:cooling solution for a propulsion component, from material requirements to thermal and fluid simulation and manufacturing feasibility, reviewed by your tutor.
Flexible format:100% online, no fixed timetables, compatible with full-time work.
Capstone project

Build it end to end

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

Define the component
Set the component, its operating conditions and the material temperature requirements.
Select cooling techniques
Choose between internal, film, effusion or transpiration cooling and suitable coatings.
Design the geometry
Produce the geometric design of the cooling solution, considering additive manufacturing.
Simulate and assess
Run the thermal and fluid simulation and evaluate the performance cost.
Final project
Compare alternatives and present the chosen solution in a report reviewed by your tutor.
Career opportunities

Where this takes you

Turbine Cooling EngineerHeat Transfer EngineerThermal CFD EngineerHigh-Temperature Materials EngineerElectric Propulsion Thermal Management EngineerPropulsion Researcher
Admissions & scholarships

Requirements

  • No prior qualification is required.
  • Internet connection and a computer capable of running the programme software.
  • English sufficient to read technical standards.

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 300 hours over 3 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with Ansys CFX, STAR-CCM+, COMSOL Multiphysics, Ansys Mechanical, nTop, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute certificate, awarded on passing the continuous assessment and the final project. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.

Yes. Modules passed are recognised in a higher programme in the same area (postgraduate diploma or master's). Ask about the recognition policy when you enrol.

No prior qualification is required: you need an internet connection, a computer able to run the programme software and English sufficient to read technical standards.

Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.

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