School / Prep
ENSPIMA
Internal code
AP8SASRM
Description
Objectives
The aim of this teaching unit is to acquire the concepts and methods essential to the dimensioning of aeronautical structures.
Skills acquired
Be able to formulate a problem with its boundary conditions, approach it in a simple way, solve it and conduct a critical analysis of the result
Validate a model by comparing its predictions with experimental results and appreciate the limits of validity of a model
Use CAD tools (Computer Aided Design) integrating trade expertise
Be able to dimension a metal or composite structure in statics.
Identify the main families of materials and their properties.
Choose a material for a mechanical part, taking into account its functionality and physical, technical and economic constraints.
Interpret experimental data to envisage their modeling.
Competencies acquired level supervised mastery
Design and dimension mechanical systems
Communicate and work as part of a team Manage and lead a work unit or project group
Competencies being acquired
Mobilize a broad field of fundamental and technical sciences related to aeronautical and space mechanical systems, and have the analytical and synthesis skills associated with them
Choose and implement analysis and characterization methods relevant to mechanical systems
Design, dimension, implement and test a metallic or composite repair/modification
Have a global systems approach to mechanical systems Reason in a context of international regulatory constraints
Integrate into a professional environment in France or abroad Communicate orally and in writing in English
Evaluate one's own skills and manage one's career path
Teaching hours
- CMLectures8h
- TDTutorial20h
- PRACTICAL WORKPractical work9h
Mandatory prerequisites
AP7SASRM
AP5SIMAI
Syllabus
Contents
This course is structured in two parts.
Strength of materials
Basic notions of strength of materials:
Presentation of aeronautical structures and their dimensioning
Practical work: Introduction to the RDM software of the IUT du Mans and application to simple cases
Project: Sizing of an aeronautical mechanism, e.g. an aircraft door opening/closing system
Continuous media mechanics
Notions of stress
Notions of deformation
Behavioral laws of continuous media
TD: Applications of the concepts covered in class (4 sessions)
Finite element modeling
Introduction to the finite element method
1D elements
Dynamic calculation
Applications of the concepts covered in class (4 sessions)
TP : Application to FE software (4 sessions)
Teaching method
Teaching associated with Moodle online resources and online resources associated with the different software used in practical work
Integrated lecture/TD approach with in-class demonstrations
Strong connection between TDs and TPs.
Further information
Specialization: Aeronautical structures
Assessment of knowledge
Initial assessment / Main session - Tests
Type of assessment | Type of test | Duration (in minutes) | Number of tests | Test coefficient | Eliminatory mark in the test | Remarks |
---|---|---|---|---|---|---|
Final inspection | Written | 120 | 0.4 | without document | ||
Final inspection | Written | 120 | 0.4 | without document | ||
Continuous control | Machine work | 0.2 |
Second chance / Catch-up session - Tests
Type of assessment | Type of test | Duration (in minutes) | Number of tests | Test coefficient | Eliminatory mark in the test | Remarks |
---|---|---|---|---|---|---|
Final test | Written | 120 | 0.4 | without document | ||
Final test | Written | 120 | 0.4 | without document |