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Instruction on FEM Analysis Using MSC Nastran/Patran. Linear and Buckling Analysis

Reinforcing Beams on a Fugelage Structure Using very Thin Skin, Fixed at one End

Seminararbeit 2014 34 Seiten

Ingenieurwissenschaften - Luft- und Raumfahrttechnik

Zusammenfassung

The aim of this exercise is to perform a Finite Element Analysis using M.Sc. Patran/Nastran tool on a hyperboloid structure. The structure is a part of the tail section of PW-6U glider. Angular straight Beams are created as re-enforcement of the structure. The load is taken from the manual of the PW-6U glider and a Linear and a Buckling analysis is performed to see the effect of the beams on the structural strength.

Details

Seiten
34
Jahr
2014
ISBN (eBook)
9783656966234
Dateigröße
2.6 MB
Sprache
Englisch
Katalognummer
v298375
Institution / Hochschule
Uniwersytet Warszawski (Universität Warschau) – FACULTY OF POWER AND AERONAUTICAL ENGINEERING
Note
5
Schlagworte
MSC NASTRAN/PATRAN FEM ANALYSIS

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Titel: Instruction on FEM Analysis Using MSC Nastran/Patran. Linear and Buckling Analysis