eVTOL Conceptual Design Course
About our
EVTOL Conceptual Design Course
This course delves into the initial design of electric vertical takeoff and landing (eVTOL) vehicles, combining aerodynamics, electric propulsion, and aircraft architecture. It explores configuration selection, performance analysis, and weight and power estimation using simulation and 3D modeling tools. The course also covers the integration of flight control systems and compliance with safety regulations, preparing participants to develop innovative concepts in the field of urban air mobility.
This course delves into the initial design of electric vertical takeoff and landing (eVTOL) vehicles, combining aerodynamics, electric propulsion, and aircraft architecture.
The course provides a solid foundation in the principles of aeronautical engineering and key eVTOL technologies, including batteries, electric motors, and thermal management systems. Emphasis is placed on the technical and economic feasibility of designs, with a focus on performance optimization and the integration of complex systems. Topics such as aircraft certification and market trends are addressed, facilitating entry into the aerospace sector.
eVTOL Conceptual 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: 2
699 $
Competencies and results
What you will learn
1. Principles of eVTOL Design and Optimization: Rotors and Aerodynamics
- Master the fundamentals of aerodynamics applied to eVTOLs, including airfoils and flow analysis.
- Understand rotor theory, design, and optimization for efficiency and stability.
- Evaluate the structural behavior of rotors, considering the loads and stresses they experience.
- Study the aerodynamic and structural phenomena related to rotors, including the vortex ring state and instability.
- Apply simulation tools (CFD, FEA) for the design and analysis of eVTOL rotors and components.
- Identify and mitigate the risks associated with fatigue and component failure in specific operating environments.
- Analyze flap-lag-torsion and whirl couplings flutterand fatigue.
- Size laminates in composites, unions and bonded joints with FE.
- Implement damage tolerance and NDT (UT/RT/thermography).
2. Design, Analysis and Performance of Rotors for eVTOL
2. Design, Analysis, and Performance of Rotors for eVTOL
- Fundamentals of rotor aerodynamics and its application in eVTOL.
- CFD modeling and simulation of rotors for design optimization.
- Advanced structural analysis of rotors: flap-lag-torsion, whirl flutter, and fatigue.
- Design of rotors considering composite materials and their properties.
- Dimensioning of laminates in composites, joints, and bonded joints with FEA analysis.
- Implementation of damage tolerance methodologies and NDT techniques (UT/RT/thermography).
- Evaluation of rotor performance: efficiency, noise, and vibration.
- Studies of Practical cases and examples of rotor design for eVTOLs.
Design optimization for different eVTOL configurations.
Specialized software tools for rotor analysis and design.
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. Optimization and Advanced Rotor Modeling for eVTOL
- Delve into the analysis of crucial aeromechanical couplings: flap-lag-torsion, essential for rotor stability and control; the whirl flutter phenomenon, which can lead to structural instability; and fatigue factors, vital for long-term durability.
- Master the dimensioning of complex laminated structures using finite element (FE) methods, focusing on the use of advanced composites. This includes the detailed design of joints and bonded joints, ensuring structural integrity and efficiency.
- Gain practical experience in applying damage tolerance methodologies to assess safety in the presence of damage. Furthermore, learn to use non-destructive testing (NDT) techniques, such as ultrasonic testing (UT), radiography (RT), and thermography, for the inspection and verification of component integrity.
5. Analysis, Modeling and Optimization of eVTOL Rotors: Conceptual Design and Performance
- In-depth analysis of the aerodynamics of eVTOL rotors, including the study of airfoil profiles and their influence on performance.
- Evaluate the structural response of rotors under various loads, considering composite materials and advanced manufacturing techniques.
- Master the modeling of eVTOL rotors using specialized software, simulating dynamic behavior and critical flight conditions.
- Apply optimization techniques to improve efficiency and reduce rotor weight, considering factors such as blade design and rotor configuration.
- Analyze flap-lag-torsion, whirl flutter, and fatigue couplings.
- Dimension laminates in composites, joints, and bonded joints with FE.
- Implement damage tolerance and NDT (UT/RT/thermography).
Explore the conceptual design of eVTOL rotors, considering different configurations and performance requirements.
Calculate and analyze the performance of eVTOL rotors under various operating conditions, including takeoff, landing, and cruise flight.
Study the relevant regulations and standards for the design and certification of eVTOL rotors.
Understand the interaction between the rotor and the flight control system (FCS) to ensure stability and handling.
6. Advanced Modeling and Performance Analysis of eVTOL Rotors
- Master eVTOL rotor modeling, including flap-lag-torsion couplings, essential for understanding complex blade dynamics.
- Evaluate stability and performance by analyzing critical phenomena such as whirl flutter and their impact on safety and design.
- Understand rotor fatigue mechanisms and design strategies to mitigate their effect on aircraft lifespan.
- Explore the dimensioning of laminated structures in composites using finite element analysis (FEA) methods.
- Design and analyze joints and bonded joints in composites, crucial for structural integrity and efficiency.
- Apply damage tolerance analysis techniques to Ensure safety in case of failure.
Implement non-destructive testing (NDT) techniques such as UT (ultrasound), RT (radiography), and thermography for inspection and quality control.
Who this program is for:
eVTOL Conceptual Design Course
- Engineers with degrees in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or related fields.
- Experts working in OEMs of rotary-wing/eVTOL aircraft, Maintenance, Repair, and Operations (MRO) organizations, consulting firms, or technology centers.
- Professionals with experience in areas such as Flight Testing, aircraft certification, avionics, control systems, and flight dynamics who wish to specialize.
- Personnel from Aeronautical regulatory bodies/authorities and professionals involved in Urban Air Mobility (UAM) / eVTOL projects seeking to develop competencies in regulatory compliance.
Recommendations: A background in aerodynamics, systems control, and structures is suggested. Proficiency in Spanish or English at a B2+ / C1 level is required. If necessary, leveling courses are offered.
- 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. Principles of eVTOL Design and Optimization: Rotors and Aerodynamics
1.1 Basic principles of aerodynamics: lift, drag, airfoil
1.2 Introduction to eVTOL propulsion systems: rotors, propellers, ducts
1.3 Rotor design: geometry, pitch, blade arrangement
1.4 Rotor performance analysis: thrust, power, efficiency
1.5 Effects of rotor-rotor and rotor-fuselage interaction
1.6 Blade structure: materials and manufacturing
1.7 Noise and vibration considerations in rotor design
1.8 Rotor optimization methodologies
1.9 Introduction to CFD and FEM simulations in rotor design
1.10 Case studies: Design and analysis of eVTOL rotors
2. Design, Analysis, and Performance of eVTOL Rotors
2.1 Review of aerodynamic principles: blade element theory
2.2 Detailed rotor design: blade shape, twist, Sweeping
2.3 Rotor Performance Analysis Using Blade Element Theory
2.4 CFD Analysis Methods for Rotors: Steady and Transient Flow
2.5 Evaluation of Rotor Stability and Control
2.6 Structural Analysis of Rotors: Strength, Stiffness, Fatigue
2.7 Rotor Design Optimization for Different Flight Conditions
2.8 Material Selection and Manufacturing Processes for Rotors
2.9 Noise and Vibration Considerations in Design and Analysis
2.10 Case Studies: Rotor Design, Analysis, and Performance
3. Conceptual Design and Analysis of eVTOL Rotors: Performance and Modeling
3.1 Conceptual Design of eVTOL Rotors: Configuration Selection
3.2 Rotor Modeling: Blade Element Theory and Vortex Modeling
3.3 Rotor Performance Simulation: Thrust, Power, Efficiency
3.4 Rotor Design Sensitivity Analysis
3.5 Rotor Design Optimization to Meet Requirements
3.6 Design Considerations for Different Rotor Types
3.7 Modeling and simulation of complex flows
3.8 Vehicle stability and control analysis
3.9 Rotor design and analysis in crosswind conditions
3.10 Case studies: Conceptual design and analysis of rotors
4. Optimization and Advanced Modeling of Rotors for eVTOLs
4.1 Review of rotor optimization principles
4.2 Advanced optimization methodologies: genetic algorithms, shape-based optimization
4.3 Rotor modeling: reduced-order modeling, high-fidelity simulation
4.4 Advanced CFD simulation techniques for rotors
4.5 Rotor-rotor interaction analysis: aeroelasticity, aeroacoustics
4.6 Rotor design for different missions and flight profiles
4.7 Noise reduction techniques in rotor design
4.8 Fault modeling and simulation and safety analysis
4.9 Integration of rotors with the flight control system
4.10 Case studies: Optimization and advanced modeling of rotors
5. Analysis, eVTOL Rotor Modeling and Optimization: Conceptual Design and Performance
5.1 Conceptual Rotor Design: Key Configurations and Parameters
5.2 Rotor Modeling: Software and Simulation Tools
5.3 Rotor Performance Analysis: Thrust, Torque, Power, Efficiency
5.4 Rotor Design Optimization: Objectives and Constraints
5.5 Optimization Methodologies: Genetic Algorithms, Shape-Based Optimization
5.6 Sensitivity Analysis and Parametric Study
5.7 Design for Different Flight Conditions
5.8 Noise and Vibration Considerations
5.9 Rotor Integration with the Propulsion System
5.10 Case Studies: Rotor Design, Analysis, and Optimization
6. Advanced Modeling and Performance Analysis of eVTOL Rotors
6.1 Review of Rotor Modeling Principles: Blade Element Theory
6.2 Advanced Modeling: CFD, Finite Element Simulation
6.3 Rotor Performance Analysis: High-Fidelity Simulation
6.4 Analysis of Rotor Behavior in Flight Transient
6.5 Aeroelasticity Considerations
6.6 Noise and Vibration Analysis
6.7 Failure Modeling and Simulation and Safety Analysis
6.8 Rotor Design for Different Flight Scenarios
6.9 Rotor Integration with the Flight Control System
6.10 Case Studies: Advanced Modeling and Performance Analysis
7. Rotor Modeling and Simulation: Conceptual Design and eVTOL Performance
7.1 Conceptual Design of eVTOL Rotors: Key Configurations and Parameters
7.2 Rotor Modeling: Blade Element Theory, Vortex Theory
7.3 Simulation Software and Tools: Xrotor, BladeElement
7.4 Rotor Performance Simulation: Thrust, Power, Efficiency
7.5 Airflow and Load Distribution Analysis
7.6 Design for Different Flight Conditions and Regimes
7.7 Rotor Stability and Control Analysis
7.8 Noise and Vibration Considerations in Design
7.9 Integration with the Propulsion and Control System
7.10 Study Case Studies: Rotor Design and Simulation
8. Modeling and Evaluation of eVTOL Rotors: Conceptual Design and Performance
8.1 Conceptual Rotor Design: Configuration Selection
8.2 Rotor Modeling: Blade Element Theory, Vortex Modeling
8.3 Performance Simulation: Thrust, Power, Efficiency, Noise
8.4 Rotor Design for Different Flight Conditions
8.5 Stability and Control Analysis
8.6 Noise and Vibration Evaluation
8.7 Structural and Fatigue Analysis
8.8 Optimization Methodologies
8.9 Integration with the Propulsion and Control System
8.10 Case Studies: Rotor Design and Evaluation
2.2 Introduction to eVTOL Rotor Design and Analysis: Fundamental Principles
2.2 eVTOL Rotor Aerodynamics: Theory and Applications
2.3 Rotor Airfoil Design: Selection and Optimization
2.4 Rotor Flow Analysis: Methods and Simulation
2.5 eVTOL Rotor Structure and Materials
2.6 Rotor Loads and Stresses: Structural Analysis
2.7 Rotor Design: Concepts and Considerations
2.8 Rotor Performance Modeling: Key Metrics
2.9 Rotor Stability Analysis
2.20 Design for Rotor Manufacturing and Assembly
3.3 Introduction to the Conceptual Design of eVTOL Rotors
3.2 Selection of Key Parameters and Definition of Requirements
3.3 Preliminary Aerodynamic Analysis and Performance Estimation
3.4 Rotor Shape Design and Airfoil Selection
3.5 Initial Modeling and Simulation of the eVTOL Rotor
3.6 Performance Evaluation Under Different Flight Conditions
3.7 Rotor Control System Design
3.8 Noise and Vibration Considerations
3.9 Feasibility Analysis and Optimization of the Conceptual Design
3.30 Presentation and Review of the eVTOL Rotor Conceptual Design
4.4 Principles of eVTOL Rotor Optimization
4.2 Advanced Optimization Methodologies
4.3 Simulation and Analysis Tools for Optimization
4.4 Design of Experiments and Sensitivity Analysis in eVTOL Rotors
4.5 Optimization Algorithms Applied to eVTOL Rotors
4.6 Integration of Design and Operational Constraints
4.7 Multiobjective Optimization in Rotor Design
4.8 Optimization Techniques for Performance and Energy Efficiency
4.9 Case Studies: Practical Application of Optimization
4.40 Validation and Verification of Optimized Models
5.5 eVTOL Design Principles: Fundamental Concepts and Architecture
5.5 Basic Aerodynamics Applied to Rotors: Lift, Drag, and Efficiency
5.3 Rotor Design: Airfoil Selection
5.4 Initial Rotor Modeling and Simulation
5.5 Rotor Materials and Manufacturing
5.6 Stability and Control in eVTOLs
5.7 Electric Propulsion Systems: Motors and Controllers
5.8 Preliminary Performance Analysis
5.9 Safety Considerations
5.50 Introduction to Optimization
5.5 Rotor Theory: Impulse, Momentum, and Blade Elements
5.5 Detailed Rotor Design: Geometry, Torsion, and Chord Distribution
5.3 Performance Analysis: Blade Element Methods
5.4 Rotor-Rotor Interaction Effects in Multi-Rotor Configurations
5.5 Structural Analysis of Rotors: Loads and Stresses
5.6 Computational Dynamics (CFD) Methods for Rotor Analysis
5.7 Hovering and Forward Flight Performance
5.8 Noise and Vibrations in eVTOL Rotors
5.9 Sensitivity Analysis of Design Parameters
5.50 Case Studies of Rotor Design and Analysis
3.5 Conceptual Design: Defining Requirements and Specifications
3.5 Rotor Configuration Selection
3.3 Initial Rotor Sizing: Calculating Diameter and Pitch
3.4 Performance Estimation: Quick and Simplified Methods
3.5 Airfoil Selection: Criteria and Considerations
3.6 Analysis of the Influence of Weight on Design
3.7 Parametric Rotor Modeling
3.8 Hovering and Transition Flight Simulation
3.9 Design Considerations for Safety
3.50 Design Feasibility Assessment
4.5 Introduction to Optimization: Concepts and Methods
4.5 Defining Design Objectives and Constraints
4.3 Selecting Design Variables
4.4 Optimization Methods: Genetic Algorithms and Gradient-Based Optimization
4.5 Rotor Geometry Optimization
4.6 Aerodynamic Performance Optimization
4.7 Structural and Weight
4.8 Noise Optimization
4.9 Simulation and Validation of Results
4.50 Rotor Optimization Case Studies
5.5 Rotor Modeling: Blade Element Methods (BEM) and CFD
5.5 Rotor Performance Analysis: Calculation of Power, Thrust, and Efficiency
5.3 Rotor-Rotor Interaction Modeling
5.4 Hovering and Forward Flight Performance Modeling
5.5 Sensitivity Analysis of Design Parameters
5.6 Vibration and Noise Analysis
5.7 Implementation of Models in Simulation Software
5.8 Model Validation with Experimental Data
5.9 Rotor Analysis and Modeling Case Studies
5.50 Analysis of the Impact of Atmospheric Conditions
6.5 Advanced Rotor Models: Vortex Modeling and CFD
6.5 Rotor Dynamics Modeling: Modal Analysis and Aeroelasticity
6.3 Performance Analysis in Different Flight Regimes
6.4 Interaction Modeling Rotor-Fuselage
6.5 Disturbance Response Analysis
6.6 Detailed Noise and Vibration Modeling
6.7 Implementation of Advanced Models in Simulation Software
6.8 Model Validation with Experimental Data and CFD
6.9 Design Optimization with Advanced Models
6.50 Case Studies of Advanced Rotor Modeling
7.5 Simulation Software Selection: Advantages and Disadvantages
7.5 Creating the Rotor Model in Simulation Software
7.3 Configuring Flight and Simulation Conditions
7.4 Simulating Rotor Performance in Different Flight Regimes
7.5 Analysis of Simulation Results
7.6 Noise and Vibration Simulation
7.7 Disturbance Response Simulation
7.8 Validation of Simulation Results
7.9 Design Optimization Using Simulation
7.50 Rotor Simulation Case Studies
8.5 Rotor Design Evaluation Criteria
8.5 Performance Evaluation: Thrust, Power, and Efficiency
8.3 Stability and Control
8.4 Noise and Vibration Assessment
8.5 Safety Assessment
8.6 Manufacturing and Operating Cost Assessment
8.7 Sensitivity and Risk Analysis
8.8 Comparison of Different Rotor Designs
8.9 Design Report and Results Presentation
8.50 Rotor Assessment Case Studies
6.6 Introduction to Electric Propulsion and Multiple Rotors in eVTOL Design
6.2 Aerodynamic Fundamentals for Rotors in Vertical Take-Off and Landing Vehicles (eVTOLs)
6.3 Aerodynamic Design of Rotors: Airfoil, Angle of Attack, and Load Distribution
6.4 Rotor Design Principles: Selection and Configuration
6.5 Factors Influencing Rotor Performance: Efficiency and Noise
6.6 Rotor Modeling and Simulation: Basic Tools and Methods
6.7 Rotor Design and Optimization: Initial Considerations
6.8 Applications and Trends in eVTOL Design
6.9 Case Studies: Examples of eVTOL Designs and Their Rotor Configurations
6.60 Impact on the Urban Environment: Vertiports and Noise
2.6 Rotor Design Principles for eVTOLs
2.2 Aerodynamic and Structural Analysis of Rotors
2.3 Rotor Performance: Lift, Thrust, and Efficiency
2.4 Design and Analysis of Rotors for Different Rotor Configurations eVTOL
2.5 Noise Considerations in Rotor Design
2.6 Material Selection and Rotor Manufacturing
2.7 Computational Fluid Dynamics (CFD) Methods for Rotors
2.8 Design for Performance Optimization
2.9 Case Studies: Rotor Performance Analysis in eVTOLs
2.60 Rotor Testing and Validation: Wind Tunnels and Flight Testing
3.6 Conceptual Design of eVTOLs and Their Rotors
3.2 Rotor Performance Analysis: Lift, Drag, and Power Required
3.3 Rotor Modeling: Blade Element Methods (BEM) and CFD
3.4 Influence of Design Parameters on Rotor Performance
3.5 Iterative Design and Optimization of Rotors
3.6 Stability and Control Considerations in Rotor Design
3.7 Rotor Integration with the Overall eVTOL Design
3.8 Rotor Design for Different Phases of Flight
3.9 Case Studies: Conceptual Design Analysis of Rotors
3.60 Development and Evaluation of Rotor Prototypes
4.6 Optimization Techniques for Rotor Design
4.2 Performance Optimization: Maximizing Efficiency
4.3 Advanced Rotor Modeling: CFD and High-Fidelity Methods
4.4 Influence of Design Parameters on Optimization
4.5 Tools and Software for Rotor Optimization
4.6 Structural and Material Optimization
4.7 Design Sensitivity and Robustness Analysis
4.8 Multidisciplinary Design and System Optimization
4.9 Case Studies: Rotor Optimization in Different Configurations
4.60 Integrating Optimization into the Design Process
5.6 Rotor Design Analysis for eVTOLs
5.2 Advanced Aerodynamic and Structural Analysis
5.3 Rotor Modeling: Tools and Techniques
5.4 Performance Considerations: Efficiency, Noise, and Vibration
5.5 Design for Different eVTOL Configurations
5.6 Rotor Stability and Control Analysis
5.7 Optimization Methods Applied to the Design of Rotors
5.8 Integrating Rotor Design with the Propulsion System
5.9 Case Studies: Rotor Analysis and Design in eVTOLs
5.60 Designing and Evaluating Rotor Prototypes
6.6 Rotor Modeling: Advanced and High-Fidelity Methods
6.2 Performance Analysis: CFD and BEM Simulations
6.3 Rotor Design and Optimization
6.4 Vibration and Noise Modeling
6.5 Integrating Rotor Design with the Control System
6.6 Failure Modeling and Reliability Analysis
6.7 Manufacturing and Cost Considerations
6.8 Modeling Electric Propulsion Systems
6.9 Case Studies: Advanced Rotor Modeling in eVTOLs
6.60 Experimental Validation and Wind Tunnel Testing
7.6 Rotor Modeling: Simulation Tools and Methods
7.2 Simulating Rotor Behavior Under Different Flight Conditions
7.3 Conceptual Design and Performance Analysis
7.4 Noise and Vibration Simulation
7.5 Integration of Rotor Design with the Flight Control System
7.6 Rotor Design Optimization
7.7 Modeling of Electric Propulsion Systems
7.8 Failure Simulation and Reliability Analysis
7.9 Case Study: Simulation and Modeling of Rotors in eVTOLs
7.60 Experimental Validation and Flight Testing
8.6 Rotor Design for eVTOLs: Key Considerations
8.2 Performance Evaluation: Lift, Drag, Power
8.3 Design for Efficiency Optimization
8.4 Noise and Vibration Evaluation
8.5 Structural Design and Fatigue Analysis
8.6 Design for Manufacturing and Assembly
8.7 Cost and Life Cycle Assessment
8.8 Certification and Safety Considerations
8.9 Case Study: Design and Evaluation of Rotors in eVTOLs
8.60 Testing and Validation: Ground and Flight Testing
- 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”).