Introduction to Airframe Design Course
About our
Introduction to Fuselage Design Course
This course provides a solid foundation in the fundamental principles of aircraft fuselage design. Key aspects such as aerodynamics, structure, and materials are explored, covering everything from conceptual design to stability and strength considerations. The use of CAD software for modeling and preliminary analysis is introduced, and basic aircraft certification regulations are examined.
Participants will learn about material selection, optimizing fuselage shape to reduce drag and maximize efficiency, and simplified structural analysis techniques. The course is designed to provide a general, yet fundamental, understanding of the airframe design process, preparing students for more specialized training in the future. Emphasis is placed on the importance of balancing design, safety, and cost requirements in aircraft development.
Introduction to Airframe Design Course
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 2
275 $
Competencies and results
What you will learn
1. Fuselage Design and Optimization: Fundamentals and Applications
- Master the principles of fuselage design, including aerodynamics and structural strength.
- Study the aerodynamic, inertial, and maneuvering loads acting on a fuselage.
- Understand the selection of materials and manufacturing processes for aeronautical fuselages.
- Evaluate the structural integrity of fuselages using finite element analysis (FEA).
- Identify and mitigate vibrations and aeroelastic phenomena, such as flutter.
- Analyze flap-lag-torsion couplings, whirl flutter, and fatigue.
- Dimension Laminates in composites, bonded joints, and bonded joints with FE.
Implement damage tolerance and NDT (UT/RT/thermography).
Learn about design optimization to improve fuselage performance and efficiency.
Become familiar with aerospace industry regulations and standards related to fuselage design.
2. Rotor Analysis and Optimization: Design and Performance
- Evaluate rotor aerodynamics and its impact on design.
- Analyze the structural dynamics of rotors, including vibrations and stability.
- Optimize rotor design to improve performance and reduce noise.
- Apply finite element analysis (FEA) methods for rotor analysis.
- Study and mitigate the effects of erosion and wear on rotors.
- Understand composite materials and their applications in rotors.
- Design and analyze rotors for different types of aircraft and applications.
- Implement non-destructive testing (NDT) techniques for rotor evaluation.
- Develop skills in using specialized software for rotor design and analysis.
- Understand industry standards and regulations related to rotor design rotors.
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. Aerodynamic Design and Analysis of Rotors: Performance and Modeling
- Design and optimize the airfoil profile of rotors for helicopters and wind turbines.
- Apply finite element analysis (FEA) methods to simulate the structural and aerodynamic behavior of rotors.
- Evaluate rotor performance under various operating conditions, including hover, climb, and descent.
- Model airflow around rotors using specialized software.
- Understand and analyze complex aerodynamic phenomena that affect rotor performance, such as lift, drag, and torque.
- Study the influence of rotor geometry, airfoil, and other design parameters on overall performance.
- Use simulation software tools to predict rotor behavior and optimize their design.
- Analyze the interaction between rotors and other aircraft components, such as the fuselage and the wings.
Understand the principles of aeroelasticity and their impact on rotor design.
Apply optimization techniques to improve rotor performance and efficiency.
5. Fuselage Design: Introduction to Aerodynamic Modeling and Analysis
5. Fuselage Design: Introduction to Aerodynamic Modeling and Analysis
- Fundamental principles of aerodynamics for fuselage design.
- Introduction to 3D modeling software for creating fuselage models.
- Computational Fluid Dynamics (CFD) techniques and their application in design.
- Optimizing the fuselage shape to minimize drag and improve efficiency.
- Considerations regarding aircraft stability and control.
- Analysis of loads and stresses in the fuselage structure.
- Introduction to materials and manufacturing processes used in fuselages.
- Design of doors, windows, and other fuselage components.
- Aeronautical design standards and regulations.
- Presentation of case studies and practical examples.
6. Fundamentals of Fuselage Design: Modeling and Initial Analysis
- Analyze the principles of fuselage modeling, including the application of finite element analysis (FEA) methods for structural analysis.
- Understand fuselage design concepts, such as aerodynamics, stability, and control.
- Evaluate the loads and stresses acting on a fuselage, including static and dynamic loads.
- Study the influence of materials and manufacturing processes on fuselage design.
- Model and analyze aspects related to fatigue strength and durability of fuselages.
- Explore non-destructive testing (NDT) techniques and their application in fuselage maintenance.
- Apply the knowledge acquired in fuselage design and analysis to practical cases and engineering projects.
Who this program is for:
Introduction to Airframe Design Course
- Engineers with degrees in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or related fields.
- Specialized personnel from rotary-wing/eVTOL aircraft manufacturers (OEMs), maintenance, repair, and overhaul (MRO) companies, consulting firms, and technology research centers.
- Flight test professionals, aeronautical certification, avionics, control systems, and flight dynamics who wish to deepen their knowledge.
- Personnel from aeronautical regulatory bodies/authorities and experts in the field of Urban Air Mobility (UAM)/eVTOL who need to acquire skills in regulatory compliance.
- 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 Conceptual Design and Initial Considerations
1.2 Preliminary Design: Shape and Main Components
1.3 Material Selection and Manufacturing Processes
1.4 Basic Aerodynamic Considerations
1.5 Stability and Control: Fundamental Principles
1.6 Structural Loads and Preliminary Analysis
1.7 Weight and Balance Estimation
1.8 Propulsion System Design
1.9 Performance Evaluation and Limitations
1.10 Introduction to Simulation and Design Tools
2.2 Rotor Design Principles: Geometry and Key Concepts
2.2 Rotor Aerodynamics: Fundamentals and Applications
2.3 Structural Analysis of Rotors: Loads and Resistance
2.4 Airfoil Design for Rotors: Selection and Optimization
2.5 Rotor Performance Analysis: Thrust, Power, and Efficiency
2.6 Rotor Design for Helicopters and VTOLs: Comparison
2.7 CFD Modeling of Rotors: Simulation and Validation
2.8 Rotor Optimization: Multidisciplinary Design
2.9 Rotor Materials and Manufacturing: Selection and Processes
2.20 Case Studies: Design and Analysis of Successful Rotors
3.3 Introduction to Airframe Aerodynamics: Fundamental Concepts
3.2 Airframe Geometry: Key Parameters and Definitions
3.3 Drag: Types and Minimization
3.4 Pressure and Force Distribution in Airframes
3.5 Laminar and Turbulent Flow: Effects and Control
3.6 Airfoils: Selection and Application
3.7 CFD Simulation Software: Introduction and Use
3.8 Wind Tunnels: Testing and Validation
3.9 Conceptual Airframe Design: Initial Considerations
3.30 Airframe Design for Different Applications: Airplanes, Helicopters, and Drones
4.4 Principles of Rotor Aerodynamics: Theory and Applications
4.2 Aerodynamic Design of Airfoils: Selection and Optimization
4.3 Flow Analysis in Rotors: Methods and Tools
4.4 Rotor Performance Modeling: Simulation and Prediction
4.5 High-Performance Rotor Design: Key Aspects
4.6 Aerodynamic Optimization of Rotors: Advanced Techniques
4.7 Rotor Stability and Control Analysis
4.8 Rotor Noise: Evaluation and Mitigation
4.9 Rotor Materials and Manufacturing: Impact on Design
4.40 Practical Applications: Case Studies and Examples
5.5 Principles of Aerodynamic Modeling and Analysis
5.5 Structural Design Considerations and Materials
5.3 Flight Control and Stability Systems
5.4 Systems and Component Integration
5.5 Performance Analysis and Design Optimization
5.6 Cockpit Design and Ergonomics
5.7 Computational Modeling and Simulation
5.8 Selection of Design Software and Tools
5.9 Fuselage Design Case Studies
5.50 Trends and Future Challenges in Fuselage Design
6.6 Fundamentals of Fuselage Geometry and Its Aerodynamic Impact
6.2 Introduction to Material Selection and Manufacturing Methods
6.3 Basic Principles of Loading and Initial Structural Analysis
6.4 Introduction to CAD Fuselage Modeling: Software and Techniques
6.5 Airflow Around Fuselages: Simulation and Visualization
6.6 Basic Performance Analysis: Drag and Lift
6.7 Systems Integration: Component Placement and Layout
6.8 Preliminary Stability and Control Assessment
6.9 Initial Design Considerations for Safety and Certification
6.60 Practical Examples and Case Studies in Fuselage 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
- Flowerplane/Rotor Optimization: CFD, structural analysis, aerodynamic optimization.
- Flight Simulation: 6DOF models, control systems, validation.
- Rotor Design: Performance analysis, modeling, and simulation.
- Stability Analysis: Control design, disturbance response, testing.
- Fuselage Design & Optimization: CFD, aerodynamic analysis, shape and drag optimization.
- Rotor Analysis & Performance: BEMT, CFD, simulation, evaluation, and optimized design.
- Rotor Modeling & Simulation: 3D modeling, performance analysis, and validation.
- Flight Dynamics: Modeling and simulation, stability and control evaluation.
- Rotor Optimization: CFD, wind tunnel, noise reduction.
- Control Systems: stability, flight protection, SIL/HIL validation.
- Aircraft Design: conversion corridor and margin analysis.
- Aeroelasticity: modal analysis, flutter, and mitigations.
DO-160: environmental testing and interference mitigation.
- Rotor Optimization: CFD, wind tunnel, acoustics.
- Stabilization: Hold, enclosure protection, SIL/HIL.
- Tiltrotor Conversion: Conversion and margin evaluation.
- Aeroelasticity: Modal analysis, flutter, mitigations.
DO-160: Environmental testing and mitigation.
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”).