Structural engineering, engineering, Other Engineering

Assignment Help:
The closed form solutions for ?max and Mmax are given on page 16.1-276 for several axial loads. Figure C-C2.2 summarizes the results for the first benchmark problem and Figure C-C2.3 summarizes the second. I want you to conduct second order analyses for both benchmark cases, using MASTAN or any other structural analysis software you choose. Here is how I want you to do it:

• Apply a uniform load of 0.2 k/ft on the first benchmark problem (as shown in the figure).
• Apply a horizontal wind load of 1.0 kips on the second benchmark problem (as shown in the figure).
• While holding these forces constant, run a series of load cases varying the axial force from 0 kips to 450 kips in increments of 50 kips (a total of 10 load cases to run) for the first benchmark problem and from 0 kips to 200 kips in increments of 20 kips (a total of 11 load cases).
• Repeat this for a 1, 10, and 20 element model for each of the two benchmark problems.

your final output
1. A table for each for the three models showing the load case, ?max, Mmax, both from the computer solutions and the exact, closed form solution, and the percent difference between the solutions (the solutions should agree within 3% for moment and 5% for deflection per the article).
2. Plots of P vs. ? and M vs. ? from your computer results for each of the three models...

Related Discussions:- Structural engineering, engineering

Assembly buildings - common fault, Assembly buildings - fire risk assessmen...

Assembly buildings - fire risk assessment: Common faults found in assembly buildings are: Combustible items left in protected routes or bedroom corridors Locked exi

Duty cycle, how to modulate duty cycles

how to modulate duty cycles

Thermo electric thermometer, how thermoelecteric thermometer is contructed ...

how thermoelecteric thermometer is contructed and how it working

Describe the antenna properties, Question: (a) Describe the following ...

Question: (a) Describe the following antenna properties / characteristics: (i) radiation pattern (ii) the main beam and beamwidth (iii) sidelobes (iv) directivity

sweep effects, In the previous discussion, we investigated the static aero...

In the previous discussion, we investigated the static aeroelastic behaviour of straight (unswept) wings. These wings are characterised by an effective decoupling of wing bending a

Full-authority digital electronic control, Full-authority digital electroni...

Full-authority digital electronic control: The supervisory control was a step toward the full-authority, fully redundant EEC. It controls all engine functions and eliminates th

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd