Basic CFD course applied to aircraft
About our
Basic CFD Course Applied to Aircraft
This course introduces the fundamentals of Computational Fluid Dynamics (CFD) and its application in the analysis of aerodynamic flows in aircraft design. It covers everything from the basic principles of fluid mechanics to the numerical simulation of complex flows, including the use of CFD software for airfoil optimization and drag prediction. It focuses on modeling relevant scenarios in aircraft design, such as lift and drag evaluation, providing a solid foundation for performance analysis and decision-making in aeronautical engineering.
The course includes practical exercises and specific examples from the aeronautical industry, preparing participants to use CFD in real-world projects. Students will learn to set up CFD simulations, interpret results, and apply the acquired knowledge to improve aircraft design and understand fluid behavior around them. This training facilitates the development of skills for professional roles such as aerodynamic engineers, aircraft designers, and CFD analysts, strengthening innovation capacity in the aerospace sector.
Basic CFD course applied to aircraft
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
380 $
Competencies and results
What you will learn
1. CFD Fundamentals for Aircraft Aerodynamic Design and Analysis
- Understand the fundamental principles of Computational Fluid Dynamics (CFD).
- Become familiar with the key concepts of aircraft aerodynamics.
- Learn to use CFD tools to simulate airflow around aircraft.
- Analyze airflow behavior under different flight conditions.
- Understand how CFD is applied to aircraft design and analysis.
- Study the impact of aircraft shape and configuration on aerodynamic performance.
- Interpret and analyze the results of CFD simulations.
- Apply CFD to optimize the aerodynamic design of aircraft.
- Understand the limitations and challenges of CFD in the aeronautical context.
- Develop practical skills in using CFD software.
CFD.
2. CFD Simulation of Flows in Aircraft: Wing, Fuselage and Component Domain
Here is the requested content:
- Prediction and analysis of complex flows around wings, fuselages, and aircraft components using CFD (Computational Fluid Dynamics) simulation.
- Modeling and simulation of aircraft aerodynamics under various flight conditions, including different speeds, angles of attack, and drift angles.
- Use of specialized CFD software for mesh creation, simulation configuration, and results analysis.
- Interpretation of CFD results, including the identification of high-pressure, low-pressure, and flow separation zones.
- Optimization of aircraft design to improve aerodynamic efficiency and reduce drag.
- Study of flow interaction with different aircraft components, such as ailerons, rudders, and stabilizers.
- Analysis of aircraft stability and control using simulations CFD.
- Application of CFD simulation for the design of new aircraft and the improvement of existing ones.
- Mastery of advanced turbulence and laminar-turbulent transition modeling techniques.
- Implementation of CFD simulation validation and verification methodologies.
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. CFD Simulation: Modeling, Analysis and Optimization of Rotors in Aircraft
4. CFD Simulation: Modeling, Analysis, and Optimization of Aircraft Rotors
Master the CFD simulation process to model complex flows around aircraft rotors.
Learn to set up and run CFD simulations using specialized software, including defining boundary conditions and meshes.
Analyze the results of CFD simulations to identify areas of high stress, flow separation, and other relevant characteristics.
Optimize aircraft rotor design using the results of CFD simulations, aiming to improve efficiency, reduce noise, and minimize drag.
Understand and apply advanced CFD simulation techniques, such as turbulence simulation and multi-phase simulation.
Model and simulate the aerodynamic performance of different types of rotors, including main rotors, tail rotors, and propellers.
Interpret and validate the
5. Application of CFD in the Design and Simulation of Aircraft Components
5. Application of CFD in the Design and Simulation of Aircraft Components
Proficiency in CFD tools to simulate airflow around aircraft components, including wings, fuselages, and propulsion systems.
Optimization of component aerodynamics, reducing drag and improving fuel efficiency.
Analysis of fluid-structure interaction (FSI) to evaluate the behavior of components under aerodynamic loads.
Simulation of complex flow phenomena such as separation, vortices, and transonic and supersonic flow.
Application of CFD in the design of flight control systems, including ailerons, rudders, and elevators.
Validation of CFD results by comparing them with experimental data and wind tunnel tests.
Simulation of aircraft engine aerodynamics, including the Analysis of internal and external flows.
Study of aeroelasticity and flutter, using CFD to predict the stability of structures.
Design and optimization of aircraft components with a focus on noise reduction and improved comfort.
Use of CFD in the analysis of icing formation and the evaluation of de-icing systems.
6. CFD Modeling and Performance Analysis in Aircraft Design
- Fundamentals of Computational Fluid Dynamics (CFD) applied to aircraft aerodynamics.
- Pre-processing: generation of computational meshes for complex aircraft models.
- Configuration and execution of CFD simulations to evaluate airflow around aircraft.
- Post-processing: analysis and interpretation of CFD results to obtain aerodynamic performance data (lift, drag, moments).
- Modeling and analysis of the performance of aeronautical components: wings, fuselages, empennages.
- Optimization of aerodynamic design using CFD, including the study of airfoils and wing configurations.
- Application of CFD in the analysis of transonic and supersonic flow.
- Simulation of complex flow phenomena: boundary layer separation, turbulence,
- Contrails.
- Integration of CFD with other aircraft design and analysis tools.
- Validation of CFD models through comparison with experimental data.
- Sensitivity analysis of design parameters and evaluation of their impact on performance.
- Study of the influence of environmental conditions (altitude, temperature) on performance.
- Application of CFD in the evaluation of propulsion system performance.
- Analysis of aircraft behavior in different flight regimes.
- Use of specialized CFD software for aircraft design.
Who this program is for:
Basic CFD course applied to aircraft
- Graduates in Aerospace Engineering, Mechanical, Industrial, Automatics or similar.
- OEM rotorcraft/eVTOL professionals, MRO, consulting, technology centers.
- Flight Test, certification, avionics, control and dynamics who seek specialization.
- Regulators/authorities and UAM/eVTOL profiles that require compliance competencies.
- 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.
1.1 Introduction to Computational Fluid Dynamics (CFD)
1.2 Principles of Aerodynamics and Fundamental Equations
1.3 Discretization and Meshing in CFD
1.4 Numerical Methods for Solving the Navier-Stokes Equations
1.5 Introduction to CFD Software: Preprocessing, Solution, and Postprocessing
1.6 Concepts of Laminar and Turbulent Flow
1.7 Turbulence Models in CFD: Selection and Application
1.8 Validation and Verification of CFD Results
1.9 CFD Applications in Aircraft Design: Examples
1.10 Best Practices and Considerations in CFD Simulation
2.2 Mesh and Boundary Conditions for Wings and Fuselages
2.2 Flow Configuration and Simulation Parameters
2.3 Pressure and Velocity Distribution Analysis
2.4 Boundary Layer and Flow Separation Study
2.5 Drag and Lift Simulation
2.6 Aerodynamic Stability Analysis
2.7 Flow Simulation around Components (Flaps, Slats)
2.8 Aerodynamic Design Optimization
2.9 Validation of Results with Experimental Data
2.20 Case Studies: Wings and Fuselages in Different Configurations
3.3 Introduction to Computational Aerodynamics (CFD) and its Fundamentals
3.2 Principles of Aircraft Aerodynamics: Lift, Drag, and Airfoils
3.3 Domain Discretization: Meshes and Meshing Techniques
3.4 Navier-Stokes Equations and Simplifications
3.5 Laminar and Turbulent Flow Solutions in CFD
3.6 Validation of CFD Results: Uncertainty and Sensitivity
3.7 CFD Tools and Software: Introduction to Platforms
3.8 Case Studies: Basic Applications of CFD in Aircraft
3.9 Best Practices in CFD for Aerodynamic Analysis
3.30 Importance of Aerodynamics in Aircraft Design
2.3 CFD Simulation of Wings: Design, Analysis, and Optimization
2.2 Flow Around Fuselages: Modeling and Drag Analysis
2.3 Wing-Fuselage Interaction: Aerodynamic Effects and Optimization
2.4 Simulation of Aircraft Components: Flaps, Slats, and Ailerons
2.5 Transonic and Supersonic Flow: Simulation and Analysis
2.6 Turbulence Models in CFD: Selection and Application
2.7 Wake and Vortex Analysis: Impact on Performance
2.8 Case Studies: Simulation of Complete Aircraft
2.9 Advanced Meshing Techniques: Hybrid and Adaptive Meshes
2.30 Interpretation of Results and Validation
3.3 CFD-Aided Aerodynamic Design: Workflow
3.2 Airfoil Design Using CFD
3.3 Wing Optimization: Shape and Lift Distribution
3.4 Fuselage Design: Drag Reduction and Efficiency Improvement
3.5 Stability and Control Analysis: Maneuvering Simulation
3.6 Control Surface Design: Flaps, Slats, and Ailerons
3.7 Propulsion System Design: Intake and Exhaust Flow
3.8 CFD Applications in Commercial Aircraft Design
3.9 CFD Applications in Aircraft Design Military
3.30 Case Studies: Aerodynamic Aircraft Design with CFD
4.3 Rotor Modeling: Theory and Applications
4.2 Rotor Flow Simulation: Steady-State and Transient Approaches
4.3 Rotor Performance Analysis: Lift, Thrust, and Power
4.4 Rotor Blade Design and Optimization with CFD
4.5 Rotor-Wake Interaction Effects: Analysis and Modeling
4.6 Helicopter and Drone Simulation: Flow in Multiple Rotors
4.7 Application of CFD in Propeller Design
4.8 Aerodynamic Rotor Noise: Simulation and Mitigation
4.9 Case Studies: Analysis of Rotors in Different Configurations
4.30 Validation of Rotor Simulation Results
5.3 CFD in the Design of Aeronautical Components: Detailed Analysis
5.2 Air Intake Design: Flow and Efficiency
5.3 Exhaust Design: Drag Reduction and Flow Mixing
5.4 Cooling System Analysis: Flow and Heat Transfer Heat
5.5 Design of Control Components: Ailerons, Rudders, and Elevators
5.6 Simulation of Landing Systems: Flow and Drag
5.7 Modeling of Propulsion Systems: Nozzle Flow
5.8 Component Optimization with CFD: Parametric Design
5.9 Applications of CFD in Aircraft Component Design
5.30 Integration of CFD into the Component Design Process
6.3 CFD Modeling for Aircraft Performance Analysis
6.2 Induced Drag and Friction Analysis
6.3 Optimizing Aircraft Shape to Reduce Drag
6.4 Performance Analysis under Different Flight Conditions
6.5 Influence of Altitude and Speed on Performance
6.6 Fuel Efficiency Evaluation Using CFD
6.7 Aircraft Stability and Control Analysis
6.8 Maneuver Simulation and Performance Evaluation
6.9 Application of CFD in Aircraft Performance Evaluation
6.30 Integration of CFD into the Design Process and Optimization
7.3 Aircraft Design with CFD: Workflow and Methodologies
7.2 Evaluation of Aircraft Aerodynamics in Various Configurations
7.3 Stability and Control Analysis Using CFD
7.4 Optimization of Wing and Fuselage Design with CFD
7.5 Design of Flight Control Systems with CFD
7.6 Evaluation of the Environmental Impact of Aircraft
7.7 Performance Analysis Under Different Flight Conditions
7.8 Simulation of Critical Flight Scenarios
7.9 Integration of CFD into the Aircraft Certification Process
7.30 Case Studies: Aircraft Design and Evaluation with CFD
8.3 CFD Analysis of Aeronautical Components: Methodologies
8.2 Optimization of Wing, Fuselage, and Control Surface Design
8.3 Analysis of Component Interactions
8.4 Simulation of Complex and Transient Flows
8.5 Design of Propulsion Systems and Performance Evaluation
8.6 Optimization of Aircraft Energy Efficiency
8.7 Stability Evaluation and aircraft control
8.8 Application of optimization techniques
8.9 Case studies: component analysis and optimization
8.30 Implementation of CFD in component design and optimization
4.4 Fundamentals of Rotor Aerodynamics and CFD Concepts
4.2 CFD Rotor Modeling: Geometry, Mesh, and Configuration
4.3 CFD Simulation of Flows in Rotors: Techniques and Methods
4.4 Analysis of CFD Results: Pressure, Velocity, and Forces
4.5 CFD Rotor Design Optimization: Methods and Tools
4.6 CFD Applications in Propeller and Turbine Design
4.7 CFD in Rotor Stability and Control Analysis
4.8 CFD Rotor Noise Simulation
4.9 Case Studies: CFD Applications in Rotor Design
4.40 Future Trends in CFD for Rotors
5.5 Fundamental Principles of CFD
5.5 Navier-Stokes Equations and Simplifications
5.3 Classical Aerodynamics: Concepts and Definitions
5.4 Boundary Layer Theory
5.5 Domain Discretization: Meshes
5.6 Solution Methods: Stability and Convergence
5.7 Introduction to CFD Software: Interface and Workflow
5.8 Validation of Results: Importance and Methods
5.5 Wing Modeling: Geometry and Meshes
5.5 Flow Simulation Around Wings: Lift and Drag Analysis
5.3 Fuselage Modeling: Design and CFD Simulation
5.4 Fuselage Flow Analysis: Pressure and Force Distribution
5.5 Component Simulation: Flaps, Slats, and Airbrakes
5.6 Wing-Fuselage Interaction: Aerodynamic Effects
5.7 Stability and Control Analysis
5.8 Techniques Advanced Meshing: Adaptation and Refinement
3.5 Aircraft Design: Aerodynamic Considerations
3.5 CFD Simulation for Preliminary Design
3.3 Flow Analysis in Complete Aircraft
3.4 Shape Optimization: Winglets and Other Components
3.5 Performance Evaluation: Range, Speed, and Efficiency
3.6 CFD Stability and Control Analysis
3.7 CFD Software Applied to Aircraft Design
3.8 Case Studies: Design and Analysis of Different Aircraft Types
4.5 Rotor Modeling: Geometry and Meshes
4.5 CFD Simulation of Rotor Flow: Thrust and Torque Analysis
4.3 Modeling Propulsion Systems: Propellers and Turbines
4.4 Rotor-Flow Interaction: Wake Effects
4.5 Propulsion Efficiency Analysis
4.6 Rotor Design: Selection and Optimization
4.7 Flow Simulation in Complex Environments
4.8 CFD Software: Applications in Helicopters and Drones
5.5 CAD Modeling and Preparation for CFD
5.5 Turbulence Model Selection
5.3 Sensitivity Analysis: Design Parameters
5.4 Topology Optimization: Generative Design
5.5 Shape Optimization: Techniques and Applications
5.6 Multiscale Flow Simulation
5.7 Validation of Optimization Results
5.8 CFD Software and Optimization Tools
6.5 Aerodynamic Performance Analysis: Drag, Lift, and Moments
6.5 Efficiency Evaluation: Lift-to-Drag Ratio
6.3 Engine and Propeller Modeling
6.4 Transient Flow Analysis
6.5 Flow Analysis with Chemical Reactions
6.6 Flow Simulation under Climatic Conditions
6.7 CFD Software: Performance Analysis and Applications
6.8 Case Studies: Analysis of Different Configurations Aircraft Design
7.5 Wing Design: Aerodynamic Design
7.5 Fuselage Design: Form and Function
7.3 Aerodynamic Control System Design
7.4 Vertical and Horizontal Stabilizer Design
7.5 Design Evaluation: Full Flow Analysis
7.6 Interference Effects Simulation
7.7 Design Validation: Virtual Wind Tunnel
7.8 CFD Software: Aircraft Design and Evaluation
8.5 CFD Analysis of Critical Components: Wings, Stabilizers
8.5 Design Optimization: Drag Reduction
8.3 Design Optimization: Lift Enhancement
8.4 Design Optimization: Stability Considerations
8.5 Design for Manufacturing: Flow Analysis
8.6 Assembly Simulation
8.7 Failure Analysis: CFD Simulation
8.8 CFD Software: Component Optimization
6.6 Introduction to CFD Modeling in Aircraft Design
6.2 Fundamentals of CFD Simulation in Aircraft Design
6.3 CFD Modeling Methodology for Aircraft
6.4 Tools and Software for CFD in Aircraft Design
6.5 Applications of CFD in Aircraft Performance Analysis
6.6 Optimizing Aircraft Design Using CFD
6.7 Validation and Verification of CFD Models
6.8 Case Studies: Application of CFD in Aircraft Design
6.9 Future Trends in CFD Modeling for Aircraft
6.60 Integrating CFD into the Aircraft Design Process
- 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.
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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”).