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· 26-30 · 31-35 · 36-40 · 41-45 · 46-50 · 51-55 · 56-60 · 61-65 · 66-70 · 71-75 · 76-80 ·FEM -Plate ,Beam and Shell Elements-Please help--OTA 104967
FEM -Plate ,Beam and Shell Elements-Please help-URGENT!!! Please see notes and ques attached
Subject:
Mechanical and Materials Engineering
Topic:
Other
Posting ID:
69435
OTA ID:
104967
FEM -Plate ,Beam and Spring Elements-Please help--OTA 104967
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Subject:
Mechanical and Materials Engineering
Topic:
Other
Posting ID:
70127
OTA ID:
104967
FEM - Plane problems - Finite element methods-urgent!!!
Attached is the problem in the file problem.pdf. There are special notes from the textbook for the questions from the textbook in notes.pdf. There are lecture notes in planeproblems.pdf.
Subject:
Mechanical and Materials Engineering
Topic:
Other
Posting ID:
71610
OTA ID:
104967
Finite element methods- Isoparametric Elements and Solution Techniques
Attached is problems in problemset4.pdf There is also a set of notes in a pdf file. (See attached files for full problem description)
Subject:
Mechanical and Materials Engineering
Topic:
Other
Posting ID:
71983
OTA ID:
104967
(See attached file for full problem description with equations and diagram) --- Practice problem for Fracture and Fatigue. Adapted from S. Suresh, Fatigue of Materials, second edition, Cambridge University Press Publishing. Consider an aircraft fuselage, existing like a cylindrical pressure vessel. Every day, this aircraft takes 6 flights, and each time, the fuselage is pressurized to a (This means the pressure DIFFERENCE between the inside and the outside.) The radius of the fuselage is . The fuselage skin is made of an aluminum alloy with thickness . Thus, you should all be able to calculate the hoop stresses in this system. Now assume that a crack of width exists... click for more
Subject:
Mechanical and Materials Engineering
Topic:
Other
Posting ID:
80059
OTA ID:
103997
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