Helicopter rotor and blade design course
About our
Helicopter Rotor and Blade Design Course
Explore the fundamental principles of aerodynamics, structures, and dynamics applied to rotor and blade design. Cover modeling and analysis using finite element method (FEM) and CFD simulations, along with the study of composite materials and manufacturing methods. Focus on performance optimization, noise reduction, and safety improvement, integrating knowledge of vibration, fatigue, and flight control to meet aviation regulations.
This course provides hands-on experience using specialized software for rotor blade design and analysis, including the application of wind tunnel testing and the evaluation of flight characteristics. The design process is covered from conceptualization to validation, preparing participants for professional roles such as rotor design engineers, performance analysts, and helicopter aerodynamics specialists, contributing to innovation in the industry.
Helicopter rotor and blade design course
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
799 $
Competencies and results
What you will learn
1. Rotor and Blade Design: Fundamentals and Advanced Simulation
- Understand the aerodynamics of rotors, including airfoils and their performance.
- Master blade design, from material selection to shape optimization.
- Use simulation software to analyze airflow and loads on rotors and blades.
- Identify and mitigate the effects of tip vortex and other sources of inefficiency.
- Evaluate the dynamic stability of rotors, including vibration analysis.
- Design rotors to meet performance and durability requirements.
- Apply optimization techniques to improve rotor and blade design.
- Estimate and reduce the noise generated by rotors.
2. Mastery of Rotor and Blade Design: Modeling, Analysis and Performance
- Delve into the modeling of rotors and blades, mastering key concepts of aerodynamics and fluid mechanics.
- Develop skills in finite element analysis (FEA) to evaluate structural integrity and aerodynamic performance.
- Understand and apply advanced 3D modeling techniques for creating accurate and optimized designs.
- Analyze failure modes and design limitations, including the study of aeroelasticity.
- Apply design methodologies for performance optimization and weight reduction in rotors and blades.
- Master the use of specialized software for the design, analysis, and simulation of rotors and blades.
- Study and analyze critical aeroelastic phenomena such as:
- Flap-lag-torsion couplings
- Whirl flutter
- Fatigue
- Gain experience in the dimensioning of laminated structures in composite materials, including:
- Design and analysis of laminates
- Analysis of bonded joints and bonded joints using FEA
- Learn and apply damage management techniques and non-destructive testing (NDT):
- Implementation of damage tolerance
- Use of NDT tests (UT/RT/thermography)
- Evaluate and optimize the aerodynamic performance of rotors and blades using CFD simulations.
- Integrate knowledge of materials, manufacturing, and processes to optimize design and production.
3. Comprehensive user-oriented design and validation (from modeling to manufacturing)
You will learn to integrate the entire product development process, from initial model conception to final validation, applying user-centered methodologies. You will develop skills in parametric design, ergonomics, simulation, sustainable materials, 3D visualization, and manufacturing management, ensuring efficient, safe solutions that meet current industry standards.
4. Aerodynamic Design and Analysis of Rotors and Blades for Helicopters
- Explore the aerodynamic design and analysis of helicopter rotors and blades.
- Understand the fundamental principles of rotor aerodynamics, including lift, drag, and efficiency.
- Study different blade geometries and their effects on helicopter performance.
- Analyze flap-lag-torsion couplings, crucial for rotor stability.
- Investigate the whirl flutter phenomenon, a critical vibration instability.
- Evaluate the fatigue of materials and structures under cyclic loading.
- Learn to dimension laminates in composites, optimizing the strength-to-weight ratio.
- Design and analyze bonded joints using Finite element (FE) analysis.
Apply damage tolerance methodologies to predict and control damage propagation.
Become familiar with non-destructive testing (NDT) techniques (UT/RT/thermography) for non-destructive inspection.
Use specialized software for aerodynamic and structural simulation of rotors.
Interpret simulation and analysis results, making informed design decisions.
Explore the latest trends in rotor design, such as next-generation blades and active control technologies.
Understand the certification requirements and safety regulations applicable to helicopters.
5. Rotor and Blade Engineering: Design, Analysis and Aerodynamic Performance
5. Rotor and Blade Engineering: Design, Analysis, and Aerodynamic Performance
- Fundamentals of rotor aerodynamics: actuator disk theory, steady and transient flow.
- Rotor modeling and simulation: specialized software, finite element analysis (FEA).
- Aerodynamic blade design: airfoil selection, chord and twist distribution, flow separation control.
- Blade structural analysis: composite materials, stress and strain analysis, failure criteria.
- Aerodynamic performance evaluation: thrust, power, and efficiency calculations, vibration analysis.
- Vibration control system design: dampers, active control systems.
- Design optimization: genetic algorithms, multi-objective optimization.
- Failure and service life analysis: fatigue modeling, inspection, and maintenance.
- Case studies: examples of design and analysis of helicopter rotors, wind turbines, and drones.
- Design for manufacturing and assembly: manufacturing considerations, material and process selection.
- Legislation and regulations: design and certification requirements, safety standards.
6. Design, Modeling and Optimization of Helicopter Rotors and Blades
- Delve into the analysis of crucial dynamic couplings: flap–lag–torsion.
- Study the whirl flutter phenomenon and its mitigation in rotor design.
- Evaluate and manage fatigue of materials in blades and rotors, optimizing service life.
- Master the dimensioning of advanced laminates manufactured with composites.
- Learn to design and analyze the integrity of joints, including bonded joints, using FEA (Finite Element Analysis).
- Apply damage tolerance methodologies to ensure structural safety.
- Understand and apply techniques of Non-Destructive Testing (NDT) such as Ultrasonic Testing (UT), Radiography (RT), and Thermography for rotor inspection.
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Who this program is for:
Helicopter rotor and blade design course
- Graduates in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or related fields.
- Professionals from OEM rotorcraft/eVTOL, MRO, consulting, technology centers.
- Flight Testing, certification, avionics, control, and dynamics seeking specialization.
- Regulators/authorities and UAM/eVTOL professionals requiring compliance skills.
Recommended qualifications: foundation in aerodynamics, control, and structures; ES/EN B2+/C1. We offer bridging tracks if you need them.
- Standards-driven curriculum: you will work with CS-27/CS-29, DO-160, DO-178C/DO-254, ARP4754A/ARP4761, ADS-33E-PRF from the first module.
- Accreditable laboratories (EN ISO/IEC 17025) with rotor bench, EMC/Lightning pre-compliance, HIL/SIL, vibrations/acoustics.
- Evidence-oriented TFM: safety case, test plan, compliance dossierand operational limits.
- Mentored by industry: teachers with experience in rotorcraft, tiltrotor, eVTOL/UAM and flight test.
- Flexible modality (hybrid/online), international cohorts and support from SEIUM Career Services.
- Ethics and security: safety-by-design approach, cyber-OT, DIH and compliance as pillars.
1. Introduction to Rotor and Propeller Design
1.1 Fundamentals of Rotor Aerodynamics: Lift, Drag, and Airflow
1.2 Blade Element Theory: Cross-Section Analysis
1.3 Blade Geometry Design: Planform, Torsion, and Airfoil
1.4 CFD Simulation Concepts for Rotors
1.5 Blade Structures and Materials: Selection and Design
1.6 Rotor Performance Analysis: Power Requirement, Efficiency, and Noise
1.7 Rotor Vibrations and Dynamics: Vibration Modes and Modal Analysis
1.8 Flight Control Systems and Rotor Actuators
1.9 Rotor Manufacturing and Assembly Considerations
1.10 Rotor Design Examples: Applications and Case Studies
2.2 Blade Geometry and Characteristics
2.2 3D Modeling of Rotors and Blades
2.3 Blade Aerodynamics Analysis
2.4 Performance Analysis Methods
2.5 Aerodynamic Flow Simulation
2.6 Effects of Bending and Torsion on Blades
2.7 Structural Analysis of Rotors
2.8 Rotor Design Optimization
2.9 Wind Tunnel Testing and Validation
2.20 Case Studies: Design and Analysis of Existing Rotors
3.3 Fundamentals of Helicopter Rotor Design
3.2 Rotor Aerodynamics: Theory and Practice
3.3 Rotor Structure and Materials
3.4 Performance Analysis and Simulation
3.5 Rotor Modeling and Optimization
3.6 Advanced Aerodynamic Design
3.7 Structural Design of Rotors
3.8 Material Selection and Manufacturing
3.9 Stability and Control Analysis
3.30 Rotor Integration and Testing
4.4 Fundamentals of Rotor Aerodynamics: Blade Element Theory (BEM) and Momentum Theory
4.2 Preliminary Rotor Design: Airfoil Selection, Load Distribution, and Geometry
4.3 Advanced Aerodynamic Modeling: CFD for Rotors, Transient Simulation
4.4 Rotor Performance Analysis: Thrust, Power, Efficiency, and Autogyro
4.5 Aerodynamics in Unsteady Flow: Effects of Flow Reversal, Stall, and Vibrations
4.6 Aerodynamic Design of Blades: Material Selection, Airfoils, and Load Distribution
4.7 Load and Structural Analysis: Finite Element Analysis (FEA) and Structural Design
4.8 Rotor Design Optimization: Optimization Methods and Multidisciplinary Design
4.9 Design and Analysis of Rotor Control Systems
4.40 Case Studies: Analysis of Existing Helicopters and New Designs
5.5 Fundamentals of Rotor Aerodynamics: Actuator Disk Theory and Finite Elements
5.5 Basic Aerodynamic Design of Blades: Airfoil Selection and Chord Distribution
5.3 Rotor Performance Analysis: Calculation of Thrust, Power, and Efficiency
5.4 3D Modeling of Rotors and Blades: CAD Software and Design Techniques
5.5 CFD Simulation of Flow over Rotors: Pressure and Velocity Analysis
5.6 Design for Performance Optimization: Parameter Tuning and Power Curves
5.7 Rotor Stability and Control Analysis
5.8 Blade Materials and Manufacturing: Selection and Processes
5.9 Risk Assessment and Failure Analysis in Rotors
5.50 Design of Rotors for Helicopters and Other Aerial Applications
6.6 Fundamentals of Rotor Modeling
6.2 Rotor Optimization Methods
6.3 3D Modeling of Rotors and Blades
6.4 Aerodynamic Analysis of Rotors
6.5 Rotor Performance Simulation
6.6 Helicopter Rotor Design
6.7 Material Selection and Blade Manufacturing
6.8 Structural Analysis of Blades
6.9 Rotor Control and Stability
6.60 Multidisciplinary Rotor Optimization
- Hands-on methodology: test-before-you-trust, design reviews, failure analysis, compliance evidence.
- Software (depending on licenses/partners): MATLAB/Simulink, Python (NumPy/SciPy), OpenVSP, SU2/OpenFOAM, Nastran/Abaqus, AMESim/Modelica, acoustics tools, planning toolchains DO-178C.
- SEIUM Laboratories: scale rotor bench, vibrations/acoustics, EMC/Lightning pre-compliance, HIL/SIL for AFCS, data acquisition with strain gauging.
- Standards and compliance: EN 9100, 17025, ISO 27001, GDPR.
Capstone-type projects
Admissions, fees, and scholarships
- Profile: Background in Computer Engineering, Mathematics, Statistics, or related fields; practical experience in NLP and valued information retrieval systems.
- Documentation: Updated CV, academic transcript, SOP/statement of purpose, project examples or code (optional).
- Process: Application → Technical evaluation of profile and experience → Technical interview → Review of case studies → Final decision → Enrollment.
- Fees:
- Single payment: 10% discount.
- Payment in 3 installments: No fees; 30% upon registration + 2 equal monthly payments of the remaining 35%.
Monthly payment: available with a 7% commission on the total; annual review.
Scholarships: based on academic merit, financial need, and promoting inclusion; agreements with companies in the sector for partial or full scholarships.
See “Calendar & Calls for Applications,” “Scholarships & Grants,” and “Fees & Financing” in the SEIUM mega-menu.
Do you have any questions?
Our team is ready to help you. Contact us, and we will respond as soon as possible.
F. A. Q
Frequently asked questions
Yes, we have international certification
Yes: experimental models, real data, applied simulations, professional environments, real case studies.
It is not mandatory. We offer leveling tracks and tutoring.
Completely. It covers e-propulsion, integration, and emerging regulations (SC-VTOL).
Recommended. There are also internal challenges and consortiums.
Yes. Online/hybrid modality with planned labs and visa support (see “Visa & Residence”).