Jan 22, 2020   11:42 p.m. Zora
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Ing. Martin Garan, PhD.
Identification number: 10008
University e-mail: martin.garan [at] stuba.sk
 
Odborný asistent CSc.,PhD. - Institute of applied mechanics and mechatronics (FME)

Contacts     Graduate     Lesson     Final thesis     Supervised theses     Conferences     

Basic information

Basic information about a final thesis

Type of thesis: Bachelor thesis
Thesis title:The stress-strain analysis of the aircraft wing structure
Written by (author): Ing. Matej Boďa
Department: Institute of applied mechanics and mechatronics (FME)
Thesis supervisor: Ing. Martin Garan, PhD.
Opponent:Ing. Matúš Pliš, PhD.
Final thesis progress:Final thesis was successfully defended.


Additional information

Additional information about the final thesis follows. Click on the language link to display the information in the desired language.

Language of final thesis:English

Slovak        English

Title of the thesis:The stress-strain analysis of the aircraft wing structure
Summary:The topic of the bachelor thesis was devoted to the stress-strain analysis of the airplane wing structure. To perform the stress-strain analysis was used the FEM method that was provided by software Ansys. Within the work was used created model of the wing in the CATIA system, which was used as the model for the FEM analysis. There were used beam as well as shell elements for the wing structure in the CATIA model. There was described the way of creating of the model of the wing using the CATIA model in detail in the work as well as the way how to create the individual parts of the structure and its following discretization. The results of the analysis are presented in the graphical form from the Ansys program as displacements and also the stress distributed on the wing structure for different operational loading.
Key words:FEM, Wing structure, Ansys

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