CourseDefense, Military Engineering & Land Systems Applications open

Helicopter Aerodynamics Course: An Academic Approach

Online 300-hour course in helicopter aerodynamics from an academic perspective. 6 modules covering ADS-33E-PRF (helicopter flying qualities), CS-29 (large helicopters, EASA) and MATLAB. Assigned tutor and open enrolment.

Duration300 h
ModeOnline
Start datesSet by the faculty
AwardSEIUM Institute certificate

Helicopter Aerodynamics Course: An Academic Approach — 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$1,240 (Canadian dollar), with instalments and employer sponsorship available.

Relevant bodies in Canada

  • Department of National Defence (DND)
  • Defence Research and Development Canada (DRDC)
  • Canadian Association of Defence and Security Industries (CADSI)
  • Public Services and Procurement Canada

Typical roles

  • Defence Systems Engineer
  • Land Systems Engineer
  • Systems Integration Engineer
  • Sustainment Engineer

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.

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Learning outcomes

What you will be able to do

01

Explain the physical principles of helicopter flight.

02

Apply momentum theory and blade element theory to the rotor.

03

Calculate performance in hover, climb and forward flight.

04

Analyse the stability and control of the helicopter.

05

Identify critical phenomena such as vortex ring state and retreating blade stall.

06

Relate design and test requirements to operations.

07

Develop an aerodynamic study of a helicopter.

Profile

Who it's for

  • Helicopter aerodynamics engineer who wants to specialise in Helicopter Aerodynamics from an academic approach.
  • Performance engineer who wants to specialise in Helicopter Aerodynamics from an academic approach.
  • Flight mechanics engineer who wants to specialise in Helicopter Aerodynamics from an academic approach.
  • Flight test engineer who wants to specialise in Helicopter Aerodynamics from an academic approach.
  • Rotor dynamics analyst who wants to specialise in Helicopter Aerodynamics from an academic approach.
  • Researcher in rotary-wing aircraft who wants to specialise in Helicopter Aerodynamics from an academic approach.
  • Graduates in engineering or science seeking to enter the helicopter industry.
Standards & tools

What you'll work with

  • ADS-33E-PRF (helicopter flying qualities)
  • CS-29 (large helicopters, EASA)
  • CS-27 (small helicopters, EASA)
  • ISO 2533 (standard atmosphere)
  • 14 CFR Part 29 (FAA)
  • AC 29-2C (certification guidance for transport category helicopters)
Syllabus

6 modules · 300 h

  1. 1.1Essential differences from fixed wing
  2. 1.2The rotor understood as a rotating wing
  3. 1.3Lift, drag and torque reaction
  4. 1.4Collective, cyclic and pedal controls
  5. 1.5The swashplate and how it transmits the command to the blade
  6. 1.6Anti-torque rotor and its alternatives
  7. 1.7Configurations: single rotor, tandem, coaxial and intermeshing
  8. 1.8Vocabulary and reference axes
  9. 1.9Helicopter-specific instrumentation
  10. 1.10Exercise: tracing a control input from the cockpit to the blade
  1. 2.1Momentum theory and the actuator disc
  2. 2.2Blade element theory
  3. 2.3Hover and induced power
  4. 2.4Ground effect and how far it extends
  5. 2.5Forward flight and lift asymmetry
  6. 2.6Flapping, drag and pitch variation
  7. 2.7Flow over the rotor disc and reverse flow regions
  8. 2.8Compressibility on the advancing blade
  9. 2.9Retreating blade stall
  10. 2.10Practice: calculating the power required in hover
  1. 3.1Power required versus airspeed curve
  2. 3.2Characteristic speeds and endurance
  3. 3.3Hover ceiling in and out of ground effect
  4. 3.4Effect of weight, altitude and temperature
  5. 3.5Performance charts and how to read them
  6. 3.6Vertical climb and its limitations
  7. 3.7Autorotation: principle and energy management
  8. 3.8Height-velocity diagram and the unsafe zone
  9. 3.9Power margin and flight planning
  10. 3.10Practice: solving a complete performance problem
  1. 4.1Static and dynamic stability
  2. 4.2Off-axis couplings
  3. 4.3Stability augmentation systems
  4. 4.4Ground resonance
  5. 4.5Vortex ring state and how to recover from it
  6. 4.6Tail rotor loss of effectiveness
  7. 4.7Vibrations and their rotor origin
  8. 4.8Blade loads and fatigue life
  9. 4.9Rotor noise and noise reduction options
  10. 4.10Practice: analysing an incident caused by an aerodynamic phenomenon
  1. 5.1Rotor design parameters
  2. 5.2Blade profiles and twist
  3. 5.3Blade materials and construction
  4. 5.4Blade balancing and tracking
  5. 5.5Wind tunnel and flight tests
  6. 5.6Test instrumentation
  7. 5.7Certification and applicable requirements
  8. 5.8Special operations: external load, mountain and maritime
  9. 5.9Rotor-related maintenance
  10. 5.10Practice: test plan for a blade modification
  1. 6.1Choice of aircraft and mission
  2. 6.2Performance requirements
  3. 6.3Preliminary rotor sizing
  4. 6.4Performance calculation
  5. 6.5Analysis of critical phenomena
  6. 6.6Test plan
  7. 6.7Proposed operating limitations
  8. 6.8Comparison with existing aircraft
  9. 6.9Technical report
  10. 6.10Project defence
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, making it possible to combine with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is MATLAB, XFOIL, OpenFOAM, FLIGHTLAB, in free, academic or evaluation versions. The test cases are studied using real performance calculation procedures with blade element theory, helicopter flight simulation, and analysis of published flight test data. Assessment is continuous per module plus the final integrative project.

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

Build it end to end

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

Choice of aircraft and mission

Explain the physical principles of helicopter flight.

Performance requirements

Apply momentum theory and blade element theory to the rotor.

Preliminary rotor sizing

Calculate performance in hover, climb and forward flight.

Performance calculation

Analyse the stability and control of the helicopter.

Analysis of critical phenomena

Identify critical phenomena such as vortex ring state and retreating blade stall.

Career opportunities

Where this takes you

Helicopter aerodynamics engineerPerformance engineerFlight mechanics engineerFlight test engineerRotor dynamics analystResearcher in rotary-wing aircraft
Admissions & scholarships

Requirements

  • No prior degree is required.
  • Internet connection and a computer capable of running the programme's software.
  • Sufficient Spanish to read technical regulations.

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, spread over 3 to 5 months. That is an average of 10 to 15 hours per week, compatible with a full-time job.

The work is carried out with MATLAB, XFOIL, OpenFOAM, FLIGHTLAB. Free, academic or evaluation versions are used, and the tutor indicates the free alternative where one exists.

An own diploma from SEIUM upon passing the continuous assessment and the integrative project. It is in-house training, not an official Ministry qualification.

Yes. Modules passed in a course or postgraduate diploma in the same area are recognised in the higher programme. Check the recognition policy when enrolling.

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