Course on aeroelasticity and wing vibrations
About our
Aeroelasticity and Vibration in Wings Course
Explore the complex interaction between aerodynamic forces, elasticity, and vibrations in aircraft wing design. It focuses on the analysis of aeroelasticity, structural dynamics, and vibration control, essential for flight safety and efficiency. Modeling and simulation techniques using FEM are covered, as well as methods for mitigating aeroelastic effects such as flutter and divergence.
The course provides knowledge of wing design, modal analysis, transient responses, and fatigue, preparing participants to address challenges in aircraft development. It includes hands-on practice with aeroelastic simulation tools and a study of applicable regulations relevant to the aerospace industry. The training equips aeronautical engineers and structural analysts with the skills to design robust and safe wings.
Course on aeroelasticity and wing vibrations
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
399 $
Competencies and results
What you will learn
1. Aeroelastic Analysis and Vibrational Dynamics of Wing Structures
- Master the analysis of critical aeroelastic phenomena, including flap-lag-torsion coupling, which affects wing stability and dynamic behavior, and whirl flutter, a potentially catastrophic instability. Structural fatigue analysis will also be covered.
- Acquire the ability to design and dimension advanced wing structures using composite materials. This includes dimensioning composite laminates, as well as designing joints and bonded joints, employing finite element (FE) analysis tools.
- Understand and apply damage tolerance methodologies to assess the safety and service life of structures, including the implementation of non-destructive testing (NDT) techniques such as ultrasonic testing (UT), radiography (RT), and thermography, for defect detection and structural integrity monitoring.
2. Comprehensive Control of Aeroelasticity and Vibrations in Wing Design
- Delve into the advanced analysis of aeroelastic phenomena, including the detailed study of complex couplings such as flap-lag-torsion, vital for structural stability.
- Evaluate and mitigate the effects of whirl flutter, a critical instability mode in rotors and propellers, and understand fatigue mechanisms in structural components.
- Apply state-of-the-art dimensioning methodologies for composite laminates, exploring design optimization in composite materials and analyzing the integrity of joints and bonded joints using finite element (FE) methods.
- Master damage tolerance techniques, which allow for predicting and controlling the behavior of structures under damage, and learn about non-destructive testing (NDT) methods, such as ultrasonic testing (UT) and radiography. (RT) and thermography, for early fault detection.
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. Advanced Engineering: Aeroelasticity, Vibrations and Optimal Wing Design
- Master the analysis of complex aeroelastic phenomena, including flap-lag-torsion coupling, whirl flutter instability, and the effects of fatigue on aeronautical structures.
- Apply advanced techniques for the dimensioning of aircraft components made of composite materials, such as laminates, and evaluate the integrity of joints and bonded joints using finite element (FE) analysis.
- Integrate damage tolerance methodologies and employ non-destructive testing (NDT) techniques such as ultrasonic testing (UT), radiography (RT), and thermography for the inspection and service life assessment of structures.
5. Comprehensive Understanding of Aeroelasticity and Wing Dynamics in Flight
5. Comprehensive Understanding of Aeroelasticity and Wing Dynamics in Flight
Explore and understand flutter phenomena, including its types: aeroelastic and separation.
Study the interaction between aeroelasticity and structural dynamics of wings.
Evaluate the effects of structural flexibility on the aerodynamic behavior of wings.
Identify and analyze the causes of failure related to aeroelasticity in wings.
Master finite element analysis (FEA) simulation tools for aeroelasticity.
Analyze flap-lag-torsion and whirl couplings. Flutter and fatigue.
Dimension laminates in composites, joints, and bonded joints with FE.
Implement damage tolerance and NDT (UT/RT/thermography).
Apply design techniques to mitigate the adverse effects of aeroelasticity in wing design.
Interpret and apply aerospace industry standards and regulations related to aeroelasticity.
6. Evaluation and Control of Aeroelastic Vibrations and Deformations in Wings
6. Evaluation and Control of Aeroelastic Vibrations and Deformations in Wings
- Identify and analyze critical aeroelastic phenomena: flap-lag-torsion couplings, whirl flutter, and fatigue mechanisms in wings.
- Master the dimensioning of wing structures using finite element (FE) for composite laminates, including the design of joints and bonded joints.
- Apply damage tolerance strategies and non-destructive testing (NDT) methods such as ultrasonic testing (UT), radiography (RT), and thermography for structural integrity assessment.
Who this program is for:
Course on aeroelasticity and wing vibrations
- Aerospace, Mechanical, Industrial, Automation Engineers, or related fields.
- Aeronautical industry professionals: OEM rotorcraft/eVTOL, MRO (Maintenance, Repair, and Operations), aeronautical consulting, and technology centers focused on aeronautics.
- Experts in areas such as Flight Testing, aircraft certification, avionics, control systems, and flight dynamics who wish to deepen their knowledge.
- Aeronautical regulators/authorities and professionals involved in UAM (Urban Air Mobility) or eVTOL (electric vertical takeoff and landing) projects who need to acquire specific competencies in regulatory compliance and certification.
Important Note: Prior knowledge of aerodynamics, control systems, and structures is recommended. The course is taught in Spanish and English, so a B2+ / C1 language level is suggested. We offer support programs (bridging tracks) to level knowledge if necessary.
- 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.
**Module 1 — Introduction to Airplane Aeroelasticity**
1. Introduction to Aeroelasticity: Fundamental Concepts
2. Importance of Aeroelasticity in Airplane Design
3. Types of Aeroelastic Instabilities: Divergence, Flutter, Reversal Control
4. Aeroelastic Phenomena: Aerodynamic-Structural Interaction
5. Wing Modeling: Simplifications and Approximations
6. Introduction to Structural Dynamics: Key Concepts
7. Introduction to Vibrations: Vibration Modes, Natural Frequencies
8. Analysis Methods: Finite Elements and Reduced Models
9. Aeroelastic Simulation Software: Introduction and Tools
10. Practical Applications: Examples of Aeroelastic Design and Analysis
2.2 Fundamental Principles of Aeroelasticity Applied to Wing Structures
2.2 Introduction to Wing Vibrational Dynamics: Key Concepts
2.3 Modeling and Simulation of Aeroelastic Wing Behavior
2.4 Structural Analysis Methods for Wing Design
2.5 Aerodynamic-Structural Interaction in Wing Design
2.6 Design to Avoid and Mitigate Aeroelastic Phenomena
2.7 Evaluation of Aeroelastic Stability: Flutter and Divergence
2.8 Aeroelastic Load Analysis and Structural Response
2.9 Introduction to Optimization in Aeroelastic Wing Design
2.20 Practical Applications and Case Studies in Wing Design
3.3 Introduction to Aeroelasticity and Vibrations in Wings
3.2 Fundamental Principles of Structural Dynamics Applied to Wings
3.3 Wing Modeling and Simulation: Aeroelastic Analysis
3.4 Aeroelastic Behavior: Deformation and Vibration
3.5 Techniques for Mitigating Vibrations and Deformations in Wings
3.6 Conceptual and Detailed Design: Aeroelasticity in the Design Process
3.7 Composite Materials and Their Impact on the Aeroelastic Behavior of Wings
3.8 Aeroelastic Testing and Trials: Validation of Models and Designs
3.9 Practical Applications: Wing Design Case Studies
3.30 The Future of Aeroelasticity and Vibrations in Wing Design
4.4 Introduction to Aeroelasticity and its Impact on Wing Design
4.2 Fundamentals of Structural Dynamics Applied to Wings
4.3 Analysis of Aerodynamic Loads and their Distribution
4.4 Modeling and Simulation of Aeroelastic Behavior
4.5 Optimal Wing Design to Minimize Aeroelastic Effects
4.6 Vibration Reduction Techniques in Wing Structures
4.7 Evaluation of Aeroelastic Stability and its Implications
4.8 Material Selection and Optimal Structural Configuration
4.9 Sensitivity Analysis and Multidisciplinary Optimization
4.40 Case Studies: Wing Design and Analysis in Different Aircraft
5.5 Fundamental Principles of Aeroelasticity and Airframe Dynamics
5.5 Types of Aeroelastic Deformations and Their Effects
5.3 Vibration Analysis in Airframe Structures
5.4 Aeroelastic Interaction: Structural-Aerodynamic Coupling
5.5 Modeling and Simulation of Airframe Behavior
5.6 Techniques for Mitigating Aeroelastic Problems
5.7 Design for the Prevention of Aeroelastic Instabilities
5.8 Tools and Software for Aeroelastic Analysis
5.9 Case Studies: Applications in Naval Design
5.50 Future Trends in Aeroelasticity and Airframe Dynamics
6.6 Introduction to Aeroelastic Vibration Mitigation in Wings
6.2 Analysis and Modeling Techniques for Identifying Vibration Modes
6.3 Design of Aeroelasticity-Resistant Wing Structures
6.4 Implementation of Dampers and Active Control Systems
6.5 Strategies for Reducing Flutter and Divergence
6.6 Evaluation of Dynamic Response and Structural Fatigue
6.7 Testing and Validation Methodologies for Anti-Vibration Designs
6.8 Design Considerations for Different Wing Types
6.9 Optimization of Wing Configuration to Minimize Vibrations
6.60 Case Studies: Practical Application of Control Techniques
- 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”).