Postgraduate DiplomaDefense, Military Engineering & Land Systems Applications open

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.

Duration6–8 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute diploma

Diploma in Aerodynamic Design of Tactical Aircraft — studying from Singapore

Singapore maintains a comprehensive defence sector through the Ministry of Defence and the Defence Science and Technology Agency, which develops military technologies and manages procurement. Engineering work covers land systems, ammunition, command and control, and simulation. Industry partners include ST Engineering, which supplies defence and security systems globally. Engineers here work within strict security and export control frameworks, often combining systems integration with reliability and safety engineering.

Fees for Singapore: S$1,280 (Singapore dollar), with instalments and employer sponsorship available.

Relevant bodies in Singapore

  • Ministry of Defence (MINDEF)
  • Defence Science and Technology Agency (DSTA)
  • ST Engineering
  • Singapore Institute of Defence Technology Industry Association

Typical roles

  • Defence Systems Engineer
  • Land Systems Engineer
  • Military Software Engineer
  • Defence Programme Engineer

Questions from Singapore

How does defence engineering work in Singapore, and which bodies oversee it?

Singapore's defence engineering is largely centred on the Ministry of Defence (MINDEF) and DSTA, the defence procurement and development agency, along with the Singapore Armed Forces. Engineers may register with the Professional Engineers Board (PEB). SEIUM's qualifications are private, not state degrees, and not accredited by any national body, so recognition for defence roles depends on the employer or relevant authority.

Who employs defence and land systems engineers in Singapore?

Main employers include MINDEF, DSTA, the SAF, and defence industry companies including ST Engineering. Access to many roles requires security clearance and citizenship or residency rules, so check eligibility early. Employers focus on proven competence and clearance status. Your final project can illustrate technical capability, but it does not replace these requirements.

Is the course manageable alongside a job, and can employers fund it?

The programme is fully online and taught in English, with an assigned technical tutor. Plan for a heavy workload: 1,900 hours for a master's, 800 for a postgraduate diploma, or 300 for a specialist course. Fees are payable in instalments, and employer sponsorship is possible, which is common in defence-linked organisations, though approval is up to them.

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Learning outcomes

What you will be able to do

01

Analyse aerofoils and their behaviour.

02

Design wings taking into account sweep, aspect ratio and twist.

03

Understand transonic and supersonic phenomena.

04

Analyse flight at high angles of attack.

05

Assess aircraft stability and control.

06

Carry out validated CFD simulations.

07

Plan and interpret wind tunnel tests.

Profile

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.
Standards & tools

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
Syllabus

8 modules

  1. 1.1Potential flow theory
  2. 1.2NACA aerofoil families
  3. 1.3Boundary layer
  4. 1.4Laminar-turbulent transition
  5. 1.5Flow separation
  6. 1.6Supercritical aerofoils
  7. 1.7Reynolds number effects
  8. 1.8Polar curves
  9. 1.9The XFOIL tool
  10. 1.10Practical: aerofoil polar with XFOIL
  1. 2.1Lifting-line theory
  2. 2.2Induced drag
  3. 2.3Effect of sweep
  4. 2.4Effect of aspect ratio
  5. 2.5Vortex lattice method
  6. 2.6Delta wings
  7. 2.7Geometric and aerodynamic twist
  8. 2.8Oswald efficiency factor
  9. 2.9Wingtip devices
  10. 2.10Lab: VLM analysis in XFLR5
  1. 3.1Critical Mach number
  2. 3.2Drag divergence
  3. 3.3Area rule
  4. 3.4Shock waves
  5. 3.5Linearised supersonic theory
  6. 3.6Wave drag
  7. 3.7Supersonic leading edges
  8. 3.8Nozzles and base effects
  9. 3.9Compressible CFD
  10. 3.10Case study: area rule applied to a fuselage
  1. 4.1Leading-edge vortices
  2. 4.2Leading-edge extensions
  3. 4.3Vortex breakdown
  4. 4.4Canards
  5. 4.5Stall onset
  6. 4.6Spin
  7. 4.7Loss of control
  8. 4.8Control surfaces at high angle of attack
  9. 4.9High-angle-of-attack testing
  10. 4.10Case study: vortices of a leading-edge extension
  1. 5.1Stability derivatives
  2. 5.2Longitudinal static stability
  3. 5.3Dynamic modes
  4. 5.4Relaxed stability
  5. 5.5Fly-by-wire controls
  6. 5.6Control surfaces
  7. 5.7MIL-STD-1797A requirements
  8. 5.8Flying qualities
  9. 5.9Flight simulation
  10. 5.10Workshop: dynamic modes in MATLAB
  1. 6.1RANS equations
  2. 6.2Turbulence models
  3. 6.3Mesh generation
  4. 6.4DES and LES methods
  5. 6.5Verification and validation
  6. 6.6AGARD validation cases
  7. 6.7Full configuration
  8. 6.8Post-processing
  9. 6.9High-performance computing
  10. 6.10Lab: RANS simulation with SU2
  1. 7.1Subsonic and transonic tunnels
  2. 7.2Aerodynamic balances
  3. 7.3PIV velocimetry
  4. 7.4Pressure-sensitive paints
  5. 7.5Wall corrections
  6. 7.6Test models
  7. 7.7Flow visualisation
  8. 7.8Similarity
  9. 7.9Correlation with CFD
  10. 7.10Case study: correction of wind tunnel data
  1. 8.1Aerodynamic requirements
  2. 8.2Aerofoil selection
  3. 8.3Wing design
  4. 8.4Transonic analysis
  5. 8.5High-angle-of-attack behaviour
  6. 8.6Stability and control
  7. 8.7CFD simulation
  8. 8.8Wind tunnel test plan
  9. 8.9Report and presentation
  10. 8.10Final 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 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.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of MIL-STD-1797A, MIL-HDBK-1797B and JSSG-2001B applied to real cases, not as a theoretical annex.
Industry software:XFOIL, XFLR5, SU2, OpenVSP and Ansys Fluent, in free, academic or evaluation versions.
Final project:An aerodynamic design of a tactical aircraft, from aerofoil selection to CFD simulation and a wind tunnel test plan, 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.

Set aerodynamic requirements
Define the requirements and select aerofoils using XFOIL polars.
Design the wing
Design the wing and analyse it with the vortex lattice method in XFLR5.
Analyse transonic and high-alpha behaviour
Apply the area rule and study high-angle-of-attack behaviour and stability.
Simulate and plan testing
Run a RANS CFD simulation with SU2 and prepare a wind tunnel test plan.
Final project
Deliver the complete aerodynamic design report and presentation, reviewed by your tutor.
Career opportunities

Where this takes you

Aerodynamics engineerCFD specialistWind tunnel test engineerFlight mechanics engineerAircraft design engineerAerodynamics researcher
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 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 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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