Diploma in Aerodynamic Design of Tactical Aircraft
Online postgraduate diploma of 800 hours in aerodynamic design of tactical aircraft: 8 modules covering aerofoil and wing aerodynamics, transonic and supersonic flow, high angle of attack, stability and control, CFD and wind tunnel testing, with an assigned technical tutor.
Diploma in Aerodynamic Design of Tactical Aircraft — studying from Canada
Canada's defence sector is centred on procurement and sustainment through the Department of National Defence and Defence Research and Development Canada. Industrial activity spans land vehicles, naval systems, avionics and electronics, with firms in Ontario, Québec, Nova Scotia and British Columbia. Companies such as General Dynamics Land Systems Canada and Lockheed Martin Canada are notable employers, alongside a broad base of small and medium suppliers. Engineers work on systems integration, vehicle protection, logistics and sustainment, operating within strict security and export control frameworks.
Fees for Canada: C$1,400 (Canadian dollar), with instalments and employer sponsorship available.
Relevant bodies in Canada
Typical roles
Questions from Canada
Which Canadian bodies or processes govern defence engineering recognition?
Defence engineering in Canada often involves government procurement and security clearances, and engineers typically hold provincial Professional Engineer licences where a title is required. SEIUM's qualifications are private and not official state degrees or accredited by a national body, so they do not confer licensing or clearance. Recognition is for employers or the relevant body to decide, so verify this first.
Would Canadian defence or land systems employers accept this training?
Canadian defence employers and contractors generally rely on security clearance, licensing and demonstrated experience. A private qualification may support your application, but it is unlikely to replace those requirements, and its acceptance is up to each employer. A SEIUM final project can help show applied skill, so discuss expectations with prospective employers early.
Can I study remotely while working, and what are the costs and language demands?
Yes, the programmes are fully online, so you can study from Canada or elsewhere without a student visa, and fit sessions around work. Specialist courses are 300 hours, postgraduate diplomas 800 and master's 1,900. Teaching is in English, supported by an assigned technical tutor. Fees are payable in instalments, and employer sponsorship may be available.
Take the controls.
Run a real engineering trade-off from this field. Move the sliders, watch the model react in real time and beat the challenge.
What you will be able to do
Analyse aerofoils and their behaviour.
Design wings taking into account sweep, aspect ratio and twist.
Understand transonic and supersonic phenomena.
Analyse flight at high angles of attack.
Assess aircraft stability and control.
Carry out validated CFD simulations.
Plan and interpret wind tunnel tests.
Who it's for
- Aerodynamics engineers.
- CFD specialists applying simulation to complete aircraft configurations.
- Wind tunnel test engineers.
- Flight mechanics engineers.
- Aircraft design engineers.
- Aerodynamics researchers.
- Engineering or science graduates seeking to enter the aerospace industry.
What you'll work with
- MIL-STD-1797A (flying qualities of piloted aircraft)
- MIL-HDBK-1797B (flying qualities handbook)
- JSSG-2001B (air vehicle joint service specification guide)
- AIAA G-077-1998 (verification and validation of CFD simulations)
- ISO 2533:1975 (standard atmosphere)
- XFOIL
- XFLR5
- SU2
- OpenVSP
- Ansys Fluent
8 modules
1.1Potential flow theory1.2NACA aerofoil families1.3Boundary layer1.4Laminar-turbulent transition1.5Flow separation1.6Supercritical aerofoils1.7Reynolds number effects1.8Polar curves1.9The XFOIL tool1.10Practical: aerofoil polar with XFOIL
2.1Lifting-line theory2.2Induced drag2.3Effect of sweep2.4Effect of aspect ratio2.5Vortex lattice method2.6Delta wings2.7Geometric and aerodynamic twist2.8Oswald efficiency factor2.9Wingtip devices2.10Lab: VLM analysis in XFLR5
3.1Critical Mach number3.2Drag divergence3.3Area rule3.4Shock waves3.5Linearised supersonic theory3.6Wave drag3.7Supersonic leading edges3.8Nozzles and base effects3.9Compressible CFD3.10Case study: area rule applied to a fuselage
4.1Leading-edge vortices4.2Leading-edge extensions4.3Vortex breakdown4.4Canards4.5Stall onset4.6Spin4.7Loss of control4.8Control surfaces at high angle of attack4.9High-angle-of-attack testing4.10Case study: vortices of a leading-edge extension
5.1Stability derivatives5.2Longitudinal static stability5.3Dynamic modes5.4Relaxed stability5.5Fly-by-wire controls5.6Control surfaces5.7MIL-STD-1797A requirements5.8Flying qualities5.9Flight simulation5.10Workshop: dynamic modes in MATLAB
6.1RANS equations6.2Turbulence models6.3Mesh generation6.4DES and LES methods6.5Verification and validation6.6AGARD validation cases6.7Full configuration6.8Post-processing6.9High-performance computing6.10Lab: RANS simulation with SU2
7.1Subsonic and transonic tunnels7.2Aerodynamic balances7.3PIV velocimetry7.4Pressure-sensitive paints7.5Wall corrections7.6Test models7.7Flow visualisation7.8Similarity7.9Correlation with CFD7.10Case study: correction of wind tunnel data
8.1Aerodynamic requirements8.2Aerofoil selection8.3Wing design8.4Transonic analysis8.5High-angle-of-attack behaviour8.6Stability and control8.7CFD simulation8.8Wind tunnel test plan8.9Report and presentation8.10Final project: final review with the tutor
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 it fits around your job.
Each module combines theory, guided reading of the original standard and applied exercises. The working software is XFOIL, XFLR5, SU2, OpenVSP and Ansys Fluent, in free, academic or evaluation versions. Practice is based on real procedures for wind tunnel testing, full-configuration CFD simulations and dynamic stability analysis. Assessment is continuous by module plus the final project.
Standards covered: MIL-STD-1797A, MIL-HDBK-1797B, JSSG-2001B, AIAA G-077-1998, ISO 2533:1975.
Build it end to end
Your final project follows the real engineering workflow, step by step, reviewed by your tutor.
Where this takes you
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 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.
Frequently asked questions
The programme totals 800 hours over 6–8 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.
You work with XFOIL, XFLR5, SU2, OpenVSP and Ansys Fluent, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.
A SEIUM Institute diploma, 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.
Prior technical training or professional experience in the sector (no university degree required), a computer able to run the 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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