Course on supersonic aerothermodynamics
About our
The Supersonic Aerothermodynamics Course delves into the study of gas flow at supersonic speeds, exploring phenomena such as shock waves, Prandtl-Meyer expansions, and compressible boundary layers. It focuses on the application of Navier-Stokes equations and numerical methods such as CFD for the analysis of supersonic flows in the design of aircraft, rockets, and supersonic wind tunnels, linking with disciplines such as propulsion and hypersonic vehicle design. The course includes the study of perfect gases, real gases, and the impact of viscosity and thermal conductivity on flow.
The training provides tools for the design and simulation of aerodynamic components operating in supersonic regimes, with special emphasis on wave drag reduction and aerodynamic performance optimization.
The shock-boundary layer interactions and their effect on the stability and control of aerial vehicles are analyzed, preparing students for roles in the research and development of advanced flight technologies, in compliance with standards such as ISO related to computational simulation.
Course on supersonic aerothermodynamics
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
599 $
Competencies and results
What you will learn
1. Advanced Fundamentals in Supersonic Aerothermodynamics: Knowledge Takeoff
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Master the key concepts of supersonic aerothermodynamics, including the Navier-Stokes equations and the Euler equations for compressible flows.
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Analyze the behavior of shock waves and Prandtl-Meyer expansions, essential for the design of high-speed aircraft.
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Study the effects of viscosity and thermal conductivity on supersonic flow, understanding boundary layer formation.
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Apply computational fluid dynamics (CFD) simulation tools to model and predict supersonic flow around different geometries.
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Understand the design principles of supersonic air intakes and evaluate their efficiency.
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Analyze the interaction between structure and flow, including aeroelastic and thermal effects.
Explore supersonic flow control techniques, such as the use of control surfaces and boundary layer control.
Understand the fundamentals of scramjet and turbojet engine design for supersonic applications.
Evaluate the performance and stability of supersonic aircraft, considering factors such as lift, drag, and directional stability.
Become familiar with the aviation safety regulations and standards applicable to supersonic aircraft.
2. Rotor Design and Analysis: Performance and Airflow Optimization
- Delve into advanced rotor analysis, including the detailed evaluation of phenomena such as flapping and ground resonance.
- Master the use of specialized software for computational fluid dynamics (CFD) simulation and aerodynamic design, optimizing blade shape for superior efficiency.
- Apply optimization techniques to reduce noise and vibrations generated by rotors, improving comfort and durability.
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. Exploration of Supersonic Phenomena: Foundations and Applications
4. Exploration of Supersonic Phenomena: Foundations and Applications
- Understand the fundamentals of supersonic aerodynamics and the Navier-Stokes equations.
- Study the design of supersonic aircraft, including wing and fuselage modeling.
- Investigate the shock wave, Prandtl-Meyer expansion, and their effects.
- Analyze transonic flow and techniques for mitigating drag.
- Evaluate the behavior of materials at high temperatures and speeds, such as titanium and ceramics.
- Master the design of supersonic wind tunnels and associated instrumentation.
- Explore the Stability and control of supersonic aircraft.
- Implement CFD (Computational Fluid Dynamics) analysis to simulate supersonic flows.
- Identify the challenges and solutions in supersonic propulsion, including ramjet and scramjet engines.
- Examine the military and civilian applications of supersonic technology, considering the environmental and economic impact.
5. Supersonic Aerothermodynamics: Flow Analysis and Component Design
5. Supersonic Aerothermodynamics: Flow Analysis and Component Design
- Mastery of the fundamentals of supersonic aerothermodynamics, including the Euler and Navier-Stokes equations.
- Comprehensive analysis of supersonic flows: shock waves, Prandtl-Meyer expansion, and flows with friction and heat transfer.
- Modeling and simulation of complex supersonic flows using advanced CFD software.
- Design and optimization of aeronautical components for supersonic speeds: air intakes, exhaust nozzles, and control surfaces.
- Study of the turbulent boundary layer in supersonic flows and its impact on design.
- Evaluation of the stability and control of supersonic aircraft.
- Introduction to drag reduction techniques in supersonic regimes supersonic aircraft.
Understanding the aeroelastic effects in supersonic flows and their mitigation.
Application of multidisciplinary design methodologies for supersonic aircraft.
Exploring the latest trends in supersonic aerodynamics research and development.
6. Rotor Modeling and Analysis: Dynamics and Efficiency in Supersonic Environments
6. Rotor Modeling and Analysis: Dynamics and Efficiency in Supersonic Environments
- Understand supersonic and transonic aerodynamics as applied to rotor design.
- Model rotor behavior under supersonic flow conditions using specialized software.
- Analyze aeroelastic interaction, including coupling between the blades and the structure.
- Evaluate energy efficiency and optimize the design to reduce fuel consumption.
- Identify and mitigate vibration and noise problems associated with high-speed rotor operation.
- Apply numerical simulation techniques (CFD, FEM) to predict rotor performance and lifespan.
- Design and analyze vibration control and noise suppression systems.
- Study the effects of blade deformation and load variation on rotor performance.
rotor.
Evaluate the impact of environmental conditions (temperature, pressure) on rotor performance.
Apply optimization methods to improve rotor design and efficiency.
Who this program is for:
Course on supersonic aerothermodynamics
- Engineers with degrees in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or other related disciplines.
- Industry specialists and technicians, including professionals from OEM rotorcraft/eVTOL, MRO (Maintenance, Repair, and Operations) companies, industry consultants, and researchers from technology centers.
- Experts in areas such as Flight Testing, aeronautical certification, avionics, systems control, and flight dynamics who wish to deepen their knowledge and specialize.
- Staff from aeronautical regulators/authorities and related profiles Professionals involved in UAM/eVTOL (Urban Air Mobility) projects who require knowledge of compliance and regulations.
Recommended Requirements: A solid foundation in aerodynamics, systems control, and structures is recommended. English proficiency (ES/EN) equivalent to B2+ or C1 is required. We offer bridging tracks for those who need to strengthen their existing knowledge.
- 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.
2.1 Fundamentals of Supersonic Aerothermodynamics: Key Concepts
2.2 Euler and Navier-Stokes Equations for Supersonic Flows
2.3 Shock and Expansion Waves: Analysis and Prediction
2.4 Design of Supersonic Nozzles: Principles and Applications
2.5 Supersonic Wind Tunnels: Methodology and Experimentation
2.6 Flow over Bodies at Supersonic Speeds: Drag and Lift
2.7 Compressibility Effects: Flow Analysis at High Speeds
2.8 Transonic Flow Analysis: Area Rules and Wing Design
2.9 Introduction to Numerical Methods for Supersonic Flows
2.10 Case Studies: Design and Optimization of Supersonic Airfoils
3.1 Principles of Rotor Design: Geometry and Parameters
3.2 Disk Theory Actuator: Flow Modeling
3.3 Rotor Blade Analysis: 2D and 3D Aerodynamics
3.4 Flow Analysis Methods: CFD and Finite Elements
3.5 Rotor Design Optimization: Performance and Noise
3.6 Rotor Tip Effects: Design and Mitigation
3.7 Rotor-Vortex Interaction: Analysis and Simulation
3.8 Rotor Design for Helicopters: Applications
3.9 Rotor Design for Drones: Efficiency and Maneuverability
3.10 Case Studies: Design and Analysis of Helical Rotors
4.1 Introduction to Supersonic Aerothermodynamics: Fundamentals
4.2 Navier-Stokes Equations and Their Application
4.3 Compressible Flow and Its Effects
4.4 Shock Waves: Formation and Behavior
4.5 Expansions of Prandtl-Meyer: Analysis and Calculation
4.6 Shock Wave Interaction: Complex Phenomena
4.7 Supersonic Boundary Layer: Development and Effects
4.8 Design of Components for Supersonic Flow: Examples
4.9 Numerical Methods for Supersonic Flows: Introduction
4.10 Applications in Aeronautical Engineering: Design and Analysis
5.1 Introduction to Supersonic Phenomena: Characteristics and Definitions
5.2 Supersonic Flow over Bodies: Drag and Lift
5.3 Shock Waves: Types and Properties
5.4 Prandtl-Meyer Expansions: Analysis and Applications
5.5 Effects of Compressibility: Flow Analysis
5.6 Interaction between Shock Waves and Boundary Layer
5.7 Design of Supersonic Nozzles: Principles and Methods
5.8 Design of Wings for Flight Supersonic: Key Aspects
5.9 Transonic Flow Analysis: Area Rules
5.10 Applications in Aerospace Engineering: Practical Examples
6.1 Supersonic Flow: Modeling and Simulation
6.2 Aeronautical Component Design: Aerodynamic Analysis
6.3 Shock Wave Modeling: Numerical Methods
6.4 Boundary Layer Analysis in Supersonic Flow
6.5 Transonic and Supersonic Flow Simulation
6.6 Nozzle Design: Optimization and Performance
6.7 Ramjet Engine Performance Analysis
6.8 CFD Analysis for Supersonic Flows
6.9 Supersonic Aircraft Design: Challenges and Solutions
6.10 Case Studies: Flow Analysis in Aeronautical Components
7.1 Rotor Modeling: Fundamentals and Principles
7.2 Computational Fluid Dynamics (CFD) for Rotors
7.3 Flow Analysis in Rotors: Methods and Techniques
7.4 Simulation of Rotating Systems: Components and Approaches
7.5 Modeling Rotor-Vortex Interaction
7.6 Energy Efficiency Analysis in Rotating Systems
7.7 Simulation of Turbulent Flow in Rotors
7.8 Rotor Design for Helicopters and Drones
7.9 Optimization of Rotating Systems: Strategies and Tools
7.10 Case Studies: Modeling and Analysis of Rotating Systems
8.1 Rotor Modeling: Principles and Fundamentals
8.2 Supersonic Aerothermodynamic Analysis
8.3 Numerical Simulation of Rotors: CFD Methods
8.4 Rotor Performance Analysis: Metrics and Evaluation
8.5 Rotor Optimization: Design and Techniques
8.6 Rotor Dynamics: Stability and Control
8.7 Modeling Rotor-Vortex Interaction
8.8 Flow Analysis in Supersonic Environments
8.9 Design of Rotors for Specific Applications
8.10 Case Studies: Performance Analysis and Rotor Design
2.2 Rotor Design Principles: Geometry and Airfoil Selection
2.2 Aerodynamic Analysis of Rotors: Disc Theory and Blade Elements
2.3 Rotor Design for Supersonic Flow: Compressibility Effects
2.4 Numerical Modeling of Rotors: CFD and Flow Simulation
2.5 Rotor Optimization: Methods and Tools
2.6 Material Selection and Rotor Manufacturing
2.7 Rotor Performance and Efficiency Analysis
2.8 Design of Rotor Control Systems
2.9 Evaluation of Rotor Stability and Control
2.20 Case Studies: Design and Analysis of Rotors in Specific Applications
3.3 Introduction to Supersonic Aerothermodynamics: Key Concepts
3.2 Fundamental Equations: Navier-Stokes and Others
3.3 Shock and Expansion Waves: Formation and Properties
3.4 Compressible Flow: Effects of the Speed of Sound
3.5 Supersonic Airfoils: Design and Characteristics
3.6 Applications in Aviation and Aerospace Engineering
3.7 Simulation Tools and Numerical Analysis
3.8 Ideal Gases and Thermodynamic Properties
3.9 Subsonic-Supersonic Transition: Transonic Flow
3.30 Practice Problems and Case Studies
2.3 Rotor Theory: Basic Principles and Operation
2.2 Blade Design: Geometry and Airfoil Selection
2.3 Airflow Analysis: Methods and Approximations
2.4 Rotor Efficiency: Influencing Factors
2.5 Ground Effect and Its Impact on Performance
2.6 Rotor Design for Different Applications
2.7 Rotor Simulation and Analysis Software
2.8 Design Optimization Methods
2.9 Rotor Design in Supersonic Environments
2.30 Case Studies and Practical Examples
3.3 Applied Equations of Supersonic Aerothermodynamics
3.2 Two-Dimensional and Three-Dimensional Supersonic Flows
3.3 Design of Supersonic Nozzles and Diffusers
3.4 Aerodynamic Drag: Sources and Mitigation
3.5 Flow Around Blunt Bodies: Characteristics and Analysis
3.6 Applications in Aircraft and Missile Design
3.7 Computational Flow Analysis (CFD) in Aerothermodynamics
3.8 Design of Supersonic Components
3.9 Advanced Materials and Technologies for Supersonic Aircraft
3.30 Aircraft Performance Simulation and Analysis
4.3 Introduction to Supersonic Phenomena: Types and Classification
4.2 Supersonic Boundary Layers: Characteristics and Effects
4.3 Interaction of shock waves and boundary layer
4.4 Interference phenomena: effects and analysis
4.5 Applications in the design of high-speed aircraft
4.6 Effects of temperature on supersonic flow
4.7 Experimental methods for supersonic research
4.8 Instrumentation and measurement techniques
4.9 Development of supersonic wind tunnels
4.30 Case studies and application examples
5.3 Analysis of supersonic flow: methods and tools
5.2 Design of supersonic air inlets
5.3 Design of supersonic nozzles
5.4 Design of supersonic wings and control surfaces
5.5 Flow-structure interaction
5.6 Numerical simulation of supersonic flow
5.7 Optimization of supersonic component design
5.8 Materials and fabrication of supersonic components
5.9 Design of supersonic propulsion systems
5.30 Case Studies and Design Examples
6.3 Modeling Rotors in Supersonic Flow: Methods and Techniques
6.2 Rotor Dynamics Analysis: Stability and Control
6.3 Effects of Compressibility on Rotor Performance
6.4 Designing Rotors for High-Speed Aircraft
6.5 Numerical Simulation of Rotors in Supersonic Environments
6.6 Aerodynamic Design of Supersonic Rotor Blades
6.7 Structural and Vibration Analysis of Rotors
6.8 Noise Reduction Methods in Supersonic Rotors
6.9 Case Studies and Practical Examples
6.30 Rotor Design Optimization
7.3 Introduction to Rotating Systems: Components and Operation
7.2 Aerothermodynamic Modeling of Rotating Systems
7.3 Effects of Compressibility on Rotating Systems
7.4 Design of Rotating Propulsion Systems
7.5 Performance Analysis of Rotating Systems
7.6 Numerical Simulation of Rotating Systems
7.7 Design of Control and Stability Systems
7.8 Applications of Rotating Systems in Aircraft
7.9 Case Studies and Examples of System Design
7.30 Optimization of Rotating System Design
8.3 Supersonic Aerothermodynamic Analysis of Rotors: Methodologies
8.2 Modeling Rotor Performance: Theory and Practice
8.3 Factors Influencing Rotor Performance
8.4 Analysis of Rotor Efficiency: Methods and Tools
8.5 Rotor Design and Optimization for Performance
8.6 Simulation of Rotor Performance
8.7 Effects of Design on Rotor Performance
8.8 Case Studies of Rotor Performance
8.9 Validation of Rotor Performance
8.30 Advanced Analysis of Rotor Performance
4.4 Shock Waves: Generation and Behavior
4.2 Prandtl-Meyer Expansions: Supersonic Flows at Corners
4.3 Flows with Friction: Boundary Layer in the Supersonic Regime
4.4 Wave Interactions: Reflection and Transmission
4.5 Supersonic Wind Tunnels: Design and Operation
4.6 Visualization of Supersonic Flows: Experimental Techniques
4.7 Aerodynamic Coefficients in the Supersonic Regime
4.8 Design of Supersonic Airfoils
4.9 Introduction to Numerical Simulation of Supersonic Flows
4.40 Applications of Supersonic Aerodynamics in Aeronautics
5.5 Introduction to Supersonic Flows and Their Characteristics
5.5 Fundamental Equations of Supersonic Aerothermodynamics
5.3 Shock Waves: Formation, Types, and Properties
5.4 Prandtl-Meyer Expansions: Analysis and Applications
5.5 Practical Applications: Supersonic Nozzles and Air Inlets
5.5 Design Principles of Rotors and Blades
5.5 Analysis of the Aerodynamic Performance of Rotors
5.3 Actuation Disk Theory and Its Applications
5.4 Flow Analysis Methods in Rotors
5.5 Optimizing Rotor Design for Efficiency
3.5 Design of Supersonic Aircraft: Key Considerations
3.5 Supersonic Propulsion: Engines and Systems
3.3 Stability and Control of Supersonic Aircraft
3.4 Advanced Materials and Technologies for Supersonic Aviation
3.5 Case Studies: Examples from Supersonic Aeronautical Engineering
4.5 Introduction to Supersonic Phenomena: Definition and Examples
4.5 Shock Wave-Boundary Layer Interaction
4.3 Effects of Viscosity on Supersonic Flows
4.4 Flow Separation Phenomena
4.5 Applications of Supersonic Phenomena in Engineering
5.5 Analysis of Supersonic Flows in Aeronautical Components
5.5 Design of Supersonic Nozzles and Diffusers
5.3 Design of Supersonic Air Inlets
5.4 Analysis of Aerodynamic Drag in Supersonic Flows
5.5 Design of Components Optimized for Supersonic Flows
6.5 Modeling Rotor Dynamics in Supersonic Environments
6.5 Analysis of Rotor Stability and Control
6.3 Numerical Simulation of Flows in Rotors
6.4 Analysis of Rotor Efficiency and Performance
6.5 Practical Applications: Optimization of Rotor Design
7.5 Modeling Rotating Systems in Supersonic Aerothermodynamics
7.5 Vibration Analysis in Rotating Systems
7.3 Design of Rotor Systems with Supersonic Considerations
7.4 Integration of Rotating Systems into Aircraft
7.5 Case Studies: Modeling of Advanced Rotating Systems
8.5 Supersonic Aerothermodynamic Analysis of Rotor Performance
8.5 Performance Analysis and Evaluation Methods
8.3 Influence of Flight Conditions on Performance
8.4 Optimizing Rotor Performance for Different Applications
8.5 Case Studies: Rotor Performance Analysis in Supersonic Scenarios
6.6 Introduction to Supersonic Aerothermodynamics and Its Applications
6.2 Navier-Stokes Equations and Their Simplification for Supersonic Flows
6.3 Shock Waves: Types, Formation, and Properties
6.4 Prandtl-Meyer Expansions
6.5 Analysis of Supersonic Flows in Nozzles and Diffusers
6.6 Effects of Viscosity and Thermal Conductivity on Supersonic Flows
6.7 Numerical Methods for Simulating Supersonic Flows
6.8 Design of Supersonic Wind Tunnels
6.9 Stability and Control of Supersonic Aircraft
6.60 Applications in Missile and Rocket Design
2.6 Fundamentals of Rotor Design
2.2 Blade Element Theory and Momentum Analysis
2.3 Aerodynamic Design of Airfoils for Rotors
2.4 Analysis of Load Distribution on the Rotor Blade
2.5 Effects of Blade Tip Flow and Vortices
2.6 Rotor Design for Helicopters and Wind Turbines
2.7 Rotor Performance Analysis: Lift, Drag, and Efficiency
2.8 Rotor Design Optimization Using Specialized Software
2.9 Rotor-Wake Interaction Study
2.60 Rotor Noise Reduction Methods
3.6 Applications of Aerothermodynamics in Supersonic Aircraft Design
3.2 Wing and Fuselage Design to Minimize Shock Wave Drag
3.3 Intake and Exhaust Systems in Supersonic Aircraft
3.4 Design of Supersonic Combustion Engines: Scramjets and Ramjets
3.5 Stability and Control Analysis of Supersonic Aircraft
3.6 Effects of Temperature and Pressure on Engine Performance
3.7 Design of Components for Thermal Management in Supersonic Aircraft
3.8 Advanced Materials and Technologies for Supersonic Aircraft
3.9 Case Studies: Historical Supersonic Aircraft and Future Projects
3.60 Environmental Impact of Supersonic Flight
4.6 Introduction to Supersonic Phenomena
4.2 Formation and Propagation of Shock Waves
4.3 Interaction of Shock Waves and Boundary Layers
4.4 Interference Phenomena in Supersonic Flows
4.5 Effects of Condensation and Cloud Formation on Supersonic Flows
4.6 Applications of Supersonic Phenomena in Engineering
4.7 Design of Experiments for the Study of Supersonic Phenomena
4.8 Methods for Visualizing Supersonic Flows
4.9 Numerical Simulation of Supersonic Phenomena
4.60 Case Studies of Applications of Supersonic Phenomena
5.6 Design of Supersonic Nozzles
5.2 Design of Supersonic Diffusers
5.3 Design of Intake Components for Supersonic Engines
5.4 Turbine Blade Design for Supersonic Flows
5.5 Analysis of Flow-Component Interaction
5.6 Selection and Design of Materials for Supersonic Components
5.7 Optimization of Component Design Using Computer Simulation
5.8 Testing and Validation of Supersonic Components
5.9 Design of Control Systems for Supersonic Flows
5.60 Safety and Reliability Considerations in Component Design
6.6 Modeling Rotor Dynamics in Supersonic Environments
6.2 Analysis of the Stability and Control of Supersonic Rotors
6.3 Effects of Compression and Shock Waves on Rotors
6.4 Simulation of Rotor-Wake Interaction in Supersonic Flows
6.5 Modeling Aeroelasticity in Supersonic Rotors
6.6 Analysis of the Vibration Response of Rotors
6.7 Design of Vibration Damping Systems
6.8 Modeling Noise Propagation in Supersonic Rotors
6.9 Optimizing Rotor Design to Minimize Noise
6.60 Numerical Model Validation Methods
7.6 Modeling Complex Rotating Systems
7.2 Analysis of the Interaction Between Rotors and Adjacent Components
7.3 Modeling Power Transmission in Rotating Systems
7.4 Fatigue and Component Life Analysis
7.5 Design of Lubrication and Cooling Systems
7.6 Modeling Failure Response and Safety Analysis
7.7 Fluid Dynamics Simulation in Rotating Systems
7.8 Heat Transfer Analysis in Rotating Systems
7.9 Optimizing the Design of Rotating Systems
7.60 Rotating System Case Studies
8.6 Aerothermodynamic Analysis of Rotors Under Supersonic Conditions
8.2 Methods for Calculating Rotor Performance
8.3 Rotor Efficiency Analysis
8.4 Effects of Compressibility on Rotor Performance
8.5 Rotor Design Optimization for Improved Performance
8.6 Analysis of the Influence of Environmental Conditions on Performance
8.7 Modeling Uncertainty and Risk in Performance Analysis
8.8 Performance Model Validation and Verification Methods
8.9 Rotor Performance Analysis Case Studies
8.60 Applications of Aerothermodynamic Analysis in Rotor Design
- 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?
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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”).