Advanced Aerodynamic Development Engineering

About our Advanced Aerodynamic Development Engineering

Advanced Aerodynamic Development Engineering (RANS/LES/DDES, adjoint, optimization)

addresses the integrated analysis of flows using hybrid turbulence models and adjoint methods for optimization in aeronautical vehicles such as helicopters and eVTOL. This specialization combines fundamentals in computational aerodynamics, advanced CFD, aeroelasticity analysis, and dynamic control, applying techniques such as RANS, LES, and DDES, together with adjoint algorithms for optimized design, overseeing efficiency, sustainability, and structural performance criteria. The curriculum incorporates simulations of transonic flow and multiphysics couplings compatible with FBW systems and international regulations.

Associated laboratories allow HIL/SIL testing and advanced signal acquisition for vibration and acoustics, ensuring traceability and safety in accordance with applicable international regulations equivalent to ARP4754A and ARP4761. The regulatory framework also considers EMC standards and protection against environmental phenomena, ensuring compliance with operational requirements of EASA CS-27/CS-29 and FAA Part 27/29. The training qualifies professionals for roles such as CFD engineer, aeroelastic analyst, flight control specialist, optimization developer, and certification engineer.

Aerodynamic Development
Advanced Aerodynamic Development Engineering

5,800 $

Skills and results

What you will learn

  • Analyze RANS, LES, and DDES couplings for flow prediction in complex aeronautical configurations, evaluating convergence criteria and numerical stability.
  • Apply adjoint and optimization for aerodynamic performance improvement, including sensitivity and gradients and handling of geometrical constraints.
  • Integrate modeling and validation strategies between RANS, LES, DDES, and optimization techniques with experimental data and benchmarks, optimizing computational resources.

2. Advanced Aerodynamic Modeling: RANS, LES, DDES, Adjoint, and Optimization

  • Analyze flap–lag–torsion couplings, whirl flutter, and fatigue.
  • Size meshes in RANS, LES, and DDES, with validity criteria and convergence.
  • Implement Adjoint and Optimization to improve aerodynamics, with sensitivity, multi-objective, and constraints.

3. Comprehensive user-oriented design and validation (from modeling to manufacturing)

You will learn to integrate the entire product development process, from model conception to final validation, applying user-centered methodologies. You will develop competencies in parametric design, ergonomics, simulation, sustainable materials, 3D visualization, and manufacturing management, ensuring efficient, safe solutions aligned with current industry standards.

4. Advanced Computational Aerodynamics Engineering: RANS, LES, DDES, Optimization, and Adjoint

  • Analyze aero-structural couplings, RANS, LES, and DDES, with emphasis on flutter, buffeting, and fatigue.
  • Size aerodynamic surfaces and structural joints in FE, evaluating meshes, convergence, and strength.
  • Implement optimization and adjoint for efficient design and weight reduction, integrating RANS, LES, and DDES for coupled predictions.

5. Advanced Aerodynamic Optimization and Simulation: RANS, LES, DDES, and Adjoint

  • Analyze hull–superstructure couplings, vibration, and fatigue under RANS, LES, DDES, and adjoint conditions.
  • Size hull geometries, hydrodynamic surfaces, and bonded joints with FE for performance and safety optimization.
  • Implement adjoint optimization for aerodynamic performance and loss reduction, integrating RANS, LES, DDES, and experimental validation.

6. Advanced Computational Aerodynamic Development: RANS, LES, DDES, Adjoint, and Optimization

  • Apply RANS and LES for aerodynamic prediction, use DDES for boundary layer and separation coupling, and utilize Adjoint to obtain design sensitivities.
  • Develop Optimization strategies based on Adjoint to reduce drag and improve performance, integrating considerations of mesh, stability, and computational cost.
  • Verify and validate CFD models against benchmarks, perform convergence analysis and post-processing, and prepare reproducible workflows for HPC.

Aerodynamic Development

Who this program is for:

Advanced Aerodynamic Development Engineering

  • Graduates in Aerospace Engineering, Mechanical, Industrial, Automation, or related fields.
  • Professionals from rotorcraft/eVTOL OEMs, MRO, consulting, technology centers.
  • Flight Test, certification, avionics, control, and dynamics professionals seeking specialization.
  • Regulators/authorities and profiles in UAM/eVTOL requiring competencies in compliance.

Recommended requirements: background 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 very first module.
  • Accreditable laboratories (EN ISO/IEC 17025) with rotor test bench, EMC/Lightning pre-compliance, HIL/SIL, vibration/acoustics.
  • TFM oriented to evidence: safety case, test plan, compliance dossier, and operational limits.
  • Industry mentoring: instructors with experience in rotorcraft, tiltrotor, eVTOL/UAM, and flight test.
  • Flexible modality (hybrid/online), international cohorts, and support from SEIUM Career Services.
  • Ethics and safety: safety-by-design approach, cyber-OT, DIH, and compliance as pillars.

1.1 Overview of Advanced Aerodynamics: objectives and scope of RANS and LES
1.2 Navier–Stokes equations and the concept of filtering in turbulence
1.3 RANS turbulence models: k-ε, k-ω, SST and their application areas
1.4 Transition and separation in RANS frameworks: prediction and limitations
1.5 LES: principles, boundary conditions, spatial and temporal resolution requirements
1.6 Hybrid RANS-LES methods: DES/DDES and blending strategies
1.7 Mesh design for RANS/LES: boundary layer resolution, cell size, and quality criteria
1.8 Numerical methods and computational performance: stability, convergence, and parallelization
1.9 Verification, validation, and uncertainty in RANS/LES simulations: benchmarks and comparisons with experimental data
1.10 Representative applications and future directions: aeronautics, naval, and aerospace

2.1 Fundamentals of CFD: Navier-Stokes equations and conservation of mass, momentum, and energy
2.2 Discretization methods: finite volumes, finite differences, and/or finite elements
2.3 Meshing and mesh quality: structured/unstructured, local refinement, quality criteria (skewness, aspect ratio)
2.4 Basic turbulence models: RANS, k-ε, k-ω, SST
2.5 CFD oriented to aerodynamics: implementation of RANS in transonic and high-Reynolds flows
2.6 LES and DDES: fundamentals, subgrid-scale models, and hybrid strategies
2.7 Adjoint and optimization in CFD: adjoint formulation, gradient calculation for optimization
2.8 Boundary conditions and wall treatment: no-slip, slip, inlet, outlet, periodicity
2.9 Post-processing and metrics: extraction of aerodynamic coefficients Cx/Cy, Cp, pressure distribution, and vorticity
2.10 Verification, validation, and uncertainty: grid convergence, code verification, comparison with experimental data, uncertainty analysis

3.1 Fundamentals of RANS and LES in advanced aerodynamics: model selection and applicability criteria
3.2 DDES and DES: hybrid approaches for transitions, separation, and complex surfaces
3.3 Adjoint and geometry optimization: gradient derivation and design strategies
3.4 Aerodynamic performance optimization: gradient-based and metaheuristic methods in aeronautical contexts
3.5 Advanced turbulence models: k-omega SST, Spalart–Allmaras, and subgrid-scale for LES
3.6 Mesh and discretization design: mesh, boundary layers, and quality criteria
3.7 Verification and validation in aerospace CFD: benchmarking, uncertainty, and compliance
3.8 Integration of CFD with MBSE/PLM: digital thread and change management in aerospace projects
3.9 Aeroelasticity and CFD-structural coupling: flutter, coupling, and robustness
3.10 Case studies: design, simulation, and evaluation of an airfoil/wing with performance and safety criteria

4.1 Introduction to Advanced Aerodynamics and CFD
4.2 Navier-Stokes equations and turbulence fundamentals
4.3 RANS turbulence models and variants (RANS, URANS, k-ε, k-ω, SST)
4.4 Large Eddy Simulation (LES) and Detached-Eddy Simulation (DDES)
4.5 Adjoints and aerodynamic design optimization
4.6 Numerical methods and discretization in CFD
4.7 Mesh design, quality criteria, and refinement
4.8 Boundary conditions, boundaries, and coupling with structures
4.9 Verification, Validation, and uncertainty in CFD
4.10 Case studies and best practices in advanced aerodynamics

5.1 Overview of Naval Advanced Aerodynamics: relevance, scope, and challenges of CFD in ships and submarines
5.2 Fundamentals of CFD for naval applications: RANS, LES, and DDES applied to external and internal flows
5.3 Adjoints and Optimization: formulation, gradients, and applications in profiles and hulls
5.4 Turbulence and transition modeling in naval fluids: k-omega, SST, and DDES/LES techniques
5.5 Simulation preparation: mesh, boundary conditions, convergence, and verification
5.6 Dynamic structure-fluid integration: FSI coupling in naval aerodynamics
5.7 Performance optimization: resistance, maneuverability, stability, and energy consumption
5.8 Aerodynamic and acoustic noise simulation in hulls and towers
5.9 Data management and traceability: MBSE/PLM for change control and model reuse
5.10 Case clinic: go/no-go with risk matrix and decision criteria

6.1 Context and scope of Advanced Computational Aerodynamics
6.2 Navier–Stokes equations and fundamentals of discretization
6.3 Introduction to RANS, LES, and DDES: concepts and differences
6.4 Adjoint and optimization in CFD: fundamentals and applications
6.5 Turbulence models: selection, calibration, and limits
6.6 Meshing techniques: quality, boundary layer resolution, and transition
6.7 Verification, validation, and cross-validation of models and solvers
6.8 CFD workflow: preprocessing, solver, and postprocessing with examples
6.9 HPC considerations and computational performance
6.10 Case study: design and evaluation of a basic aerodynamic profile with multiple CFD approaches

7.1 Fundamentals of the Navier–Stokes equations and turbulence concepts
7.2 RANS turbulence models: k-ε, k-ω, SST, and Spalart–Allmaras
7.3 Introduction to LES and SGS models: Smagorinsky, dynamic Smagorinsky, WALE
7.4 DES and low hybrid RANS-LES: principles, usage criteria, and transitions
7.5 Adjoint and sensitivity in CFD: fundamentals, formulation, and design applications
7.6 Optimization in CFD: objectives, design variables, constraints, and penalties
7.7 Mesh preparation and simulation setup: quality standards, y+, near-wall
7.8 Verification and validation in CFD: mesh testing, code verification, and benchmarking
7.9 Performance and scalability in HPC for RANS/LES: parallelism, solvers, and execution times
7.10 Naval and aeronautical case studies: hull buoyancy, propellers, and control surfaces

8.1 Introduction to Advanced Aerodynamic Modeling: overview of CFD applied to naval engineering
8.2 Fundamentals of Fluid Dynamics and Turbulence: Navier–Stokes equations, turbulence models, and resolution criteria
8.3 RANS, LES, and DDES: model selection and their impact on accuracy and computational cost in naval cases
8.4 Adjoint and Optimization in Aerodynamics: derivative calculation, sensitivities, and design strategies for hulls and propellers
8.5 Integration of aerodynamics with propulsion and structures: hull-propeller flow interaction and performance impacts
8.6 Generation and use of meshes for naval CFD: structured/unstructured meshes, near-wall resolution, and grid independence
8.7 Validation and verification of CFD models: comparison with tunnel and water test data, uncertainties
8.8 Naval Case Studies: hull optimization, drift and starboard, propeller and propulsion, noise control
8.9 Data management and workflow: MBSE/PLM, change traceability, and version control
8.10 Future trends and regulations: standards, certifications, and safety practices in naval aerodynamic modeling

9.1 Fundamentals of CFD and advanced numerical methodologies
9.2 Principles of fluid dynamics applied to naval aerodynamics
9.3 Turbulence models: RANS, LES, DDES in maritime contexts
9.4 Mesh and discretization strategies for complex aerodynamic simulations
9.5 Validation and verification of CFD models in naval applications
9.6 Introduction to optimization in naval aerodynamic design
9.7 Software tools and platforms for advanced simulation
9.8 Case studies and practical application in naval and aerospace vehicle design
9.9 Trends and advances in CFD for naval and aerospace engineering
9.10 Evaluation and analysis of results in complex aerodynamic simulations

10.1 Introduction to Advanced Computational Aerodynamics: objectives, scope, and the relationship of CFD with naval and aeronautical design
10.2 Fundamentals of the physical flow equations: Navier–Stokes, incompressible and compressible flow
10.3 Discretization methods and numerical stability: finite volumes, structured and unstructured meshing
10.4 Fundamental turbulence models: RANS, LES, and DDES; selection criteria for naval applications
10.5 Adjoint and optimization in CFD: formulation, gradients, and design strategies
10.6 Handling of boundary conditions and simulation configurations for aerodynamic flows
10.7 Verification and validation: procedures, metrics, and reference cases in naval CFD
10.8 Preprocessing and mesh generation: naval geometry, refined meshing, and quality criteria
10.9 CFD tools and environments: OpenFOAM, Fluent, STAR-CCM+, workflows, and pipelines
10.10 Introductory CFD project: planning, execution, and evaluation of results in a naval case

  • Hands-on methodology: test-before-you-trust, design reviews, failure analysis, compliance evidence.
  • Software (according to licenses/partners): MATLAB/Simulink, Python (NumPy/SciPy), OpenVSP, SU2/OpenFOAM, Nastran/Abaqus, AMESim/Modelica, acoustics tools, DO-178C planning toolchains.
  • SEIUM Laboratories: scale rotor test bench, vibration/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 information retrieval systems is valued.
  • Documentation: Updated CV, academic transcripts, SOP/purpose essay, project or code samples (optional).
  • Process: application → technical profile and experience evaluation → technical interview → practical case review → final decision → enrollment.
  • Fees:
    • Single payment: 10% discount.
    • 3-installment payment: no fees; 30% upon enrollment + 2 equal monthly payments of the remaining 35%.
    • Monthly payment: available with a 7% fee on the total; annual review.
  • Scholarships: based on academic merit, financial situation, and promotion of inclusion; agreements with industry companies for partial or full scholarships.

Check “Calendar & calls”, “Scholarships & financial aid”, 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 hold 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 consortia.

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