Course on vibrations in Rotorcraft structures
About our
Rotorcraft Structure Vibration Course
This course focuses on the study and analysis of vibrations in helicopters, addressing key topics such as structural dynamics, modal analysis, and vibration simulation. It explores vibration measurement and diagnostics techniques, along with methods for mitigating and controlling vibrations in rotors and fuselages. The course emphasizes understanding the effects of vibrations on flight safety and comfort, and how to apply solutions to improve aircraft performance and durability.
Participants will gain knowledge in the use of computational simulation tools and the operation of vibration instrumentation. Special attention is given to the application of industry standards and norms, including frequency response analysis (FRF) and experimental modal identification (EMA). The program aims to prepare participants for roles such as vibration engineers, aircraft systems analysts, and maintenance specialists in the aerospace industry.
Course on vibrations in Rotorcraft structures
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 2
399 $
Competencies and results
What you will learn
1. Vibration Analysis in Rotorcraft Structures: Fundamentals and Applications
- Understand the fundamental principles of vibration analysis applied to rotorcraft structures.
- Identify and evaluate the main sources of vibration, including imbalance, misalignment, and aerodynamic problems.
- Analyze critical vibration modes, such as flap-lag-torsion couplings, whirl flutter, and the factors that contribute to component fatigue.
- Use numerical modeling and simulation tools and techniques to predict and analyze the vibration behavior of rotorcraft structures.
- Apply concepts of structural dynamics and mechanics of materials to the design and analysis of rotorcraft components, considering dynamic loads and vibration effects.
- Dimension rotorcraft structures, including the use of laminates in composites, joints, and bonded joints, using finite element (FE) methods.
- Implement design and analysis methodologies for
- Damage tolerance, evaluating crack propagation resistance and component lifespan.
- Apply non-destructive testing (NDT) techniques, including ultrasonic testing (UT), radiography (RT), and thermography, for the inspection and evaluation of the structural integrity of rotorcraft.
- Interpret vibration analysis and NDT results, and use this information for design optimization, predictive maintenance, and improved rotorcraft safety.
- Understand the importance of applicable standards and regulations in the design, manufacture, and operation of rotorcraft, in relation to vibration analysis and structural integrity.
2. Vibration Analysis in Helicopters: Modeling, Simulation and Problem Solving
- In-depth study of helicopter vibration analysis, including modeling and simulation.
- Identify and understand critical vibration modes, such as flap-lag-torsion, that affect rotor stability.
- Evaluate the risk of phenomena such as whirl flutter and their impact on airworthiness.
- Study fatigue mechanisms in structural components and their consequences.
- Master the dimensioning of laminated structures in composite materials.
- Apply finite element (FE) analysis techniques for the design of joints and bonded joints.
- Understand the principles of damage tolerance and their application in helicopter design and maintenance.
- Implement non-invasive testing techniques Destructive testing (NDT) methods such as ultrasonic testing (UT), radiography (RT), and thermography for component inspection.
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. In-depth Study of Vibrations in Helicopters: Theory, Modeling and Control
4. In-Depth Study of Vibrations in Helicopters: Theory, Modeling, and Control
- Identify and understand the sources of vibration in helicopters.
- Analyze flap-lag-torsion, whirl flutter, and fatigue couplings.
- Apply modeling and simulation techniques for the study of vibrations.
- Develop mathematical models to predict vibration behavior.
- Dimension laminates in composites, joints, and bonded joints with FE.
- Evaluate the service life of components and structures subjected to vibrations.
- Implement damage tolerance and NDT (UT/RT/thermography).
- Apply strategies Vibration control to mitigate its effects.
Use specialized software for the analysis and design of control systems.
Understand and apply aeronautical industry standards and regulations.
5. Vibrations in Rotorcraft: Structural Modeling, Diagnosis and Mitigation
- Understand the fundamentals of rotorcraft vibrations, including their causes and effects on airworthiness and component life.
- Master advanced structural modeling of rotors, using finite element analysis (FEA) methods to simulate dynamic behavior and vibration response.
- Analyze flap-lag-torsion, whirl flutter, and fatigue couplings.
- Diagnosticate rotor vibrations using advanced data analysis techniques, including signal processing and the identification of critical vibration modes.
- Implement vibration mitigation strategies, such as the design of anti-vibration systems and the optimization of rotor configuration.
- Dimension laminates in composites, joints, and bonded joints using FE.
- Apply the principles of fracture mechanics and fatigue to evaluate the service life of rotor components and predict failures.
- Implement damage tolerance and non-destructive testing (NTT) (UT/RT/thermography).
- Become familiar with aerospace industry regulations and standards related to rotorcraft vibration and flight safety.
- Use specialized software for vibration analysis, structural modeling, and rotor simulation.
6. Advanced Vibration Modeling and Analysis in Helicopters
- Master the modeling of complex vibration systems in helicopters.
- Analyze flap-lag-torsion, whirl flutter, and fatigue couplings.
- Use specialized software to simulate and predict vibration behavior.
- Interpret the results of modal, spectral, and transient analyses.
- Dimension laminates in composites, joints, and bonded joints using FE.
- Apply Finite Element Analysis (FEA) techniques for component evaluation.
- Implement damage tolerance and NDT (UT/RT/thermography).
- Understand non-destructive testing methods and their application in the inspection of helicopters.
Who this program is for:
Course on vibrations in Rotorcraft structures
- Engineers with degrees in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or related fields.
- Technical personnel from rotorcraft/eVTOL manufacturers (OEMs), Maintenance, Repair, and Overhaul (MRO) companies, aeronautical consulting firms, and technology centers.
- Flight Testing professionals, Aeronautical Certification, Avionics, Systems Control, and Flight Dynamics who wish to deepen their knowledge and specialize.
- Representatives of organizations Aeronautical regulators and authorities, as well as professionals focused on Urban Air Mobility (UAM) / eVTOL who need to acquire compliance skills.
Recommended requirements: Basic knowledge of aerodynamics, control systems, and structures is recommended. Fluency in Spanish/English at a B2+ or C1 level is required. Bridging courses are available for those who 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 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 Fundamental Principles of Vibration Analysis in Helicopters
2.2 Types of Vibrations: Causes and Effects in Rotorcraft
2.3 Modeling Dynamic Systems in Helicopters
2.4 Vibration Simulation: Tools and Methods
2.5 Frequency and Amplitude Analysis in Critical Components
2.6 Troubleshooting: Diagnosis and Fault Location
2.7 Mitigation Strategies: Design and Modification
2.8 Practical Applications: Case Studies in Helicopters
2.9 Regulations and Standards in Vibration Analysis
2.10 Validation and Verification of Vibration Models
3.1 Vibration Dynamics Theory Applied to Rotorcraft
3.2 Mathematical Modeling of Rotating Systems
3.3 Modal and Spectral Analysis in Helicopter Components
3.4 Design of Anti-Vibration Systems: Dampers and Isolators
3.5 Optimization Design to Minimize Vibrations
3.6 Impact of Vibrations on Material Fatigue
3.7 Active and Passive Vibration Control Strategies
3.8 Transient Vibration Response Analysis
3.9 Quality and Durability Assessment in Rotorcraft
3.10 Case Studies: Design and Improvement of Anti-Vibration Systems
4.1 Fundamentals of Vibration Theory in Helicopters
4.2 Advanced Modeling of Components and Systems
4.3 Vibration Mode Analysis and Critical Frequencies
4.4 Advanced Diagnostic Techniques: Sensors and Methods
4.5 Active Vibration Control: Systems and Algorithms
4.6 Passive Vibration Control: Materials and Design
4.7 Integration of Control Systems in Helicopters
4.8 Dynamic Stability Analysis in Rotorcraft
4.9 Applications: Case Studies and Practical Examples
4.10 Future Trends in Vibration Control
5.1 Structural Modeling of Rotorcraft: Finite Elements
5.2 Vibration Analysis: Methods and Software
5.3 Fault Diagnosis: Techniques and Procedures
5.4 Vibration Mitigation: Design Strategies
5.5 Materials and Components for Vibration Reduction
5.6 Design of Isolation and Damping Systems
5.7 Implementation of Active Control Systems
5.8 Evaluation of the Effectiveness of Mitigation Strategies
5.9 Cost-Benefit Analysis of Solutions
5.10 Case Studies and Application Examples
6.1 Advanced Mathematical Modeling of Helicopters
6.2 Numerical Methods for Vibration Analysis
6.3 Modal Analysis: Theory and Applications
6.4 Time-Frequency Analysis: Tools and Techniques
6.5 Vibration Simulation in Complex Environments
6.6 Design Optimization to Minimize Vibrations
6.7 Sensitivity and Robustness Analysis
6.8 Vibration Reduction Techniques
6.9 Model Validation and Verification
6.10 Case Studies and Real-World Applications
7.1 Vibration Analysis Methodologies in Rotorcraft
7.2 Modeling and Simulation Techniques
7.3 Diagnostic and Evaluation Strategies
7.4 Vibration Mitigation System Design
7.5 Material and Component Selection
7.6 Implementation of Active Control Systems
7.7 Cost-Benefit and Feasibility Analysis
7.8 Case Studies and Best Practices
7.9 Industry Standards and Regulations
7.10 Future Trends in Vibration Mitigation
8.1 Modeling Dynamic Systems in Rotorcraft
8.2 Vibration Simulation: Methods and Software
8.3 Frequency and Amplitude Analysis
8.4 Active Control Strategies Vibration Control
8.5 Control System Design
8.6 Controller Implementation and Validation
8.7 System Stability Analysis
8.8 Control Parameter Optimization
8.9 Case Studies and Practical Applications
8.10 Future Trends in Vibration Control
2.2 Introduction to Vibration Modeling in Rotorcraft
2.2 Fundamentals of Vibration Simulation: Principles and Tools
2.3 Modeling of Structural Components: Rigid and Deformable Bodies
2.4 Modeling of Rotor Systems: Blades, Hubs, and Controls
2.5 Simulation Techniques: Modal and Transient Analysis
2.6 Model Implementation: Software and Methodologies
2.7 Results Analysis: Interpretation and Validation
2.8 Case Studies: Practical Examples and Applications
2.9 Experimental Design and Validation: Bench Tests and Flight Tests
2.20 Model Optimization: Improving Accuracy and Efficiency
3.3 Fundamentals of Vibration Theory in Rotorcraft
3.2 Introduction to Vibration Analysis in Rotor Systems
3.3 Design of Anti-Vibration Systems: Principles and Components
3.4 Vibration Mode Analysis in Rotorcraft
3.5 Vibration Mitigation Techniques: Dampers and Isolation
3.6 Rotor Blade Design to Minimize Vibrations
3.7 Vibration Modeling and Simulation in Rotorcraft
3.8 Implementation and Evaluation of Anti-Vibration Systems
3.9 Vibration Standards and Regulations in the Aviation Industry
3.30 Case Studies: Real-World Applications and Challenges
4.4 Introduction to Vibration Theory in Helicopters
4.2 Mathematical Foundations of Vibration Analysis
4.3 Modeling Vibration Systems in Helicopters
4.4 Modal and Spectral Analysis of Vibration
4.5 Vibration Sources in Helicopters: Identification and Characterization
4.6 Vibration Sensors and Measurement Techniques
4.7 Vibration-Based Fault Diagnosis
4.8 Vibration Control and Mitigation Strategies
4.9 Design of Anti-Vibration Systems
4.40 Practical Applications and Case Studies
5.5 Introduction to Vibrations in Rotorcraft: Fundamental Concepts
5.5 Vibration Theory: Amplitude, Frequency, Phase, and Normal Modes
5.3 Modeling of Single-Degree-of-Freedom (SDOF) and Multiple-Degree-of-Freedom (MDOF) Systems
5.4 Vibrations in Critical Components: Rotor Blades, Fuselage, and Transmission
5.5 Analysis of Natural Frequencies and Vibration Modes in Structures
5.6 Introduction to Experimental Modal Analysis (EMA)
5.7 Vibration Propagation and Excitation Sources in Rotorcraft
5.8 Materials and Properties: Influence on Vibrations
5.9 Vibration Detection and Measurement Methods
5.50 Software and Tools for Basic Structural Modeling
6.6 Modeling of Complex Components and Integrated Systems
6.2 Advanced Finite Element Analysis (FEA) Techniques
6.3 Modal and Frequency Response Analysis
6.4 Modeling of Complex Rotors and Transmission Systems
6.5 Vibration Simulation Under Flight and Maneuvering Conditions
6.6 Model Validation Through Experimental Testing
6.7 Design Optimization for Vibration Reduction
6.8 Fatigue and Component Life Analysis
6.9 Integration of Vibration Models with Other Systems
6.60 Case Studies and Practical Examples
- 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”).