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Aircraft Wing
H C Shomesh
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Aircraft Wing design by H C Shomesh
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Aircraft Wing test under Fatigue and Airflow, for a load of 50000N, which gave the fatigue life of 10^8 Cycles. The part is taken from online with modification it's used for analysis.
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License:
CC - Attribution
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Published
Jul 14, 2020
in
FEA Finite Element Analysis
ansys
fatigue-life
nx-nastran
Rendering Images
Siemens NX (Unigraphics)
PTC Creo Parametric
STEP/STP 3D Modeling
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