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Branch Project I. (E222121)
Departments:ústav letadlové techniky (12122)
Abbreviation:OP1Approved:11.06.2019
Valid until: ??Range:0P+2C
Semestr:Credits:2
Completion:KZLanguage:EN
Annotation
The project is focused on mastering the interconnected structural problem of aircraft and space technology. Students working in groups of two or three will be tasked with designing and calculating the aerospace design node using modern CAD and CAE software packages.
Structure
Structure of tutorial
Example Task:
Construction design of the elevator. Solution of aerodynamic load, application of aerodynamic and inertial load on the design of the elevator structure, solution of forces in the elevator control mechanism.
Literarture
https://ansyshelp.ansys.com/
https://www.plm.automation.siemens.com/global/en/support/docs.html
Requirements
No requirements.
Keywords
CFD, CAD, CAE, FEM, design, structural load
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