Physical, Mathematical, Computer and Life Sciences › Physical Sciences
This course provides a comprehensive understanding of helicopter aerodynamics, enabling learners to apply aerodynamic principles to helicopter operations. It covers the fundamental forces, rotor dynamics, and performance factors essential for safe and efficient flight.
This course is designed for helicopter pilots, maintenance engineers, and aviation professionals seeking to deepen their knowledge of helicopter aerodynamics.
None — open enrollment.
Objectives:
• Define basic aerodynamic principles relevant to helicopters
• Identify the main components of a helicopter and their functions
• Explain the concept of relative airflow and its importance
• Describe the forces acting on a helicopter in flight
• Understand the helicopter's unique flight characteristics
Topics:
• Overview of helicopter design and configuration
• Basic aerodynamic terms: lift, drag, thrust, weight
• Newton's laws of motion applied to rotorcraft
• Rotor system types: fully articulated, semi-rigid, rigid
• Forces in equilibrium: hover and forward flight
• Introduction to blade element theory
• Relative airflow and angle of attack
• Comparison with fixed-wing aerodynamics
Objectives:
• Explain how lift is generated in a hovering rotor
• Describe induced flow and its effects on rotor performance
• Calculate thrust and power required in hover
• Understand ground effect and its impact
• Analyse factors affecting hover performance
Topics:
• Momentum theory for hover
• Blade element theory in hover
• Induced velocity and inflow ratio
• Thrust coefficient and power coefficient
• Figure of merit and rotor efficiency
• Ground effect: in-ground-effect (IGE) and out-of-ground-effect (OGE)
• Effects of density altitude on hover
• Power required curves for hover
Objectives:
• Describe the airflow patterns in vertical climb and descent
• Explain autorotation and its phases
• Analyse forward flight aerodynamics including dissymmetry of lift
• Understand retreating blade stall and its implications
• Calculate power required in forward flight
Topics:
• Vertical climb: induced velocity and power
• Vertical descent: vortex ring state and settling with power
• Autorotation: entry, steady state, and flare
• Forward flight: translational lift and effective translational lift
• Dissymmetry of lift and flapping to equality
• Retreating blade stall and limitations
• Power required versus airspeed curve
• Factors affecting forward flight performance
Objectives:
• Identify the components of main and tail rotor systems
• Explain the function of cyclic, collective, and anti-torque controls
• Describe the mechanics of rotor blade articulation
• Understand the role of the swashplate
• Analyse control mixing and rigging
Topics:
• Main rotor head design: teetering, hingeless, bearingless
• Tail rotor types: conventional, Fenestron, NOTAR
• Cyclic control: pitch link and swashplate operation
• Collective control: collective lever and pitch change
• Anti-torque pedals and tail rotor thrust
• Blade articulation: flapping, lead-lag, feathering
• Control system components: push-pull tubes, cables, hydraulic actuators
• Control mixing and rigging principles
Objectives:
• Calculate hover ceiling and maximum altitude
• Determine rate of climb and best rate of climb speed
• Analyse range and endurance factors
• Understand the effects of weight, altitude, and temperature
• Interpret performance charts
Topics:
• Hover performance: IGE and OGE hover ceilings
• Climb performance: rate of climb, climb gradient
• Cruise performance: range and specific range
• Endurance: maximum endurance and fuel flow
• Factors affecting performance: gross weight, density altitude, wind
• Height-velocity diagram: avoid region
• Performance charts and data interpretation
• Limitations and safety margins
Objectives:
• Define static and dynamic stability in helicopters
• Explain the effects of the rotor on stability
• Describe control response and handling qualities
• Analyse the role of stabilizers and auxiliary surfaces
• Understand automatic flight control systems
Topics:
• Static stability: longitudinal, lateral, directional
• Dynamic stability: phugoid, Dutch roll, spiral modes
• Rotor contributions to stability: flapping, hinge offset
• Horizontal and vertical stabilizers
• Stability augmentation systems (SAS)
• Automatic flight control systems (AFCS)
• Handling qualities ratings (Cooper-Harper scale)
• Trim and control harmony
Objectives:
• Explain the sources of vibration in helicopters
• Describe rotor tracking and balancing
• Analyse ground and air resonance
• Understand the principles of vibration damping
• Apply vibration reduction techniques
Topics:
• Sources of vibration: main rotor, tail rotor, engine, transmission
• Rotor tracking: vertical and lead-lag tracking
• Rotor balancing: static and dynamic
• Ground resonance: causes and prevention
• Air resonance: coupled rotor-fuselage modes
• Vibration damping: elastomeric dampers, hydraulic dampers
• Vibration analysis and measurement
• Tuning and vibration reduction methods
Objectives:
• Identify hazardous flight conditions and their aerodynamics
• Explain the causes and recovery from vortex ring state
• Describe dynamic rollover and its prevention
• Analyse low-G conditions and mast bumping
• Understand blade sailing and ground handling
Topics:
• Vortex ring state (settling with power): causes and recovery
• Dynamic rollover: mechanics and avoidance
• Low-G conditions and mast bumping
• Retreating blade stall: symptoms and limitations
• Loss of tail rotor effectiveness (LTE)
• Blade sailing and ground resonance
• Autorotation: entry and flare technique
• Operational limitations: Vne, weight, CG
Objectives:
• Summarise key aerodynamic principles and their interplay
• Apply knowledge to real-world flight scenarios
• Analyse performance data to plan a flight
• Understand emerging technologies in rotorcraft
• Integrate aerodynamics with operational decision-making
Topics:
• Review of key concepts: lift, drag, power, stability
• Composite rotor blades and advanced airfoils
• Tiltrotor and compound helicopter aerodynamics
• Electric propulsion and UAV rotor design
• Flight planning using performance charts
• Case study: cross-country flight performance
• Human factors in helicopter operations
• Safety management and aerodynamic awareness
Hands-on practicals are essential to reinforce theoretical concepts. Learners will engage in simulator sessions, rotor track and balance exercises, and performance calculation workshops to apply aerodynamic principles in realistic scenarios.
Each delegate is assessed continuously throughout the course via daily exercises, scored practical assignments, and a final summative test at the end.
Practical assignments are observed and scored against a rubric during the practical sessions. Each delegate's practical mark is averaged into a single 100% score and contributes 30% to the final total.
Every training day ends with a multiple-choice exercise scored out of 100%. The scores from each daily exercise are averaged across the duration of the course to produce a Daily Average mark, which contributes 20% to the final total.
On the last day a final summative test is written. It is a multiple-choice paper with multiple-answer questions: each question may have more than one correct option, and a single wrong selection on a question marks the entire question wrong — no partial credit. The final test is scored out of 100% and contributes 50% to the overall mark.
| Component | Out of | Weight |
|---|---|---|
| Practical Assignments (rubric-scored) | 100% | 30% |
| Daily Average (multiple choice) | 100% | 20% |
| Final Test (multi-answer multiple choice) | 100% | 50% |
| Final Total | — | 100% |
All marks are recorded on the AATICD LMS and visible to each learner under their account.
Sign in to the LMS, open your dashboard, and your certificates appear under My Certificates. Each entry has a View / Download button and a print option.
Group discounts apply automatically — the more delegates you enrol, the greater the saving. Discounts are calculated at 3% per 5 delegates, scaling up to 40% off for 100+ delegates.
| Delegates | Discount |
|---|---|
| 5 | 3% off |
| 10 | 6% off |
| 15 | 9% off |
| 20 | 12% off |
| 25 | 15% off |
| 30 | 18% off |
| 50 | 30% off |
| 75 | 35% off |
| 100 | 40% off |
3% discount per 5 delegates, up to 40% off for 100+ delegates. Contact us for a custom group quote.
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