Aerospace computational techniques, Other Engineering

Assignment Help:

Bearing stresses are very common in aerospace engineering.  It occurs on the surface of contact between any two structural members.  Bolts, pins, and rivets are classic examples of where bearing stresses occur.  You will find these in many flight vehicles.

1900_Aerospace Computational Techniques.png

A simplified example of this is a bolt pressed against the flat surface of a bar.  This might occur during flexure testing of a material.The stresses in an elastic material under a concentrated line load P (units of [Force/Length]) are given by the following equations(Advanced Strength and Applied Elasticity, 4/e, by A.C. Ugural and S.K. Fenster, Prentice-Hall, 2003).

Using non-dimensional coordinates 394_Aerospace Computational Techniques1.png :

a) Make a three-dimensional surface plot and a two-dimensional (non-flooded) contour line plot of the absolute maximum non-dimensional shear stress2405_Aerospace Computational Techniques3.pngas a two dimensional function of x and y .Use the ranges: 2166_Aerospace Computational Techniques2.png

b)  Comment on your results.  (Don't just summarize the steps you followed.  Considering the results, discuss what the final results tell you, whether they have any interesting features, etc.)

Values for P and a are not required.  Your Mechanics of Materials textbook provides you with the equations needed to calculate the principle stresses.Your plots must make use of good plotting practices (scaling, labels, legend, etc.).  You must write a MATLAB script, saved in a .m file.  The script should include the commands to create your plots in multiple windows. To complete this assignment, turn in your MATLAB script, copies of your plots, and comments on your results.  All material should be turned in both electronically and by hard copy.  All plots submitted electronically should be in color.


Related Discussions:- Aerospace computational techniques

Fuel control system in aircraft engine, Fuel control system in Aircraft Eng...

Fuel control system in Aircraft Engine: The computer controls the fuel flow to the engine to maintain a constant rotor RPM. During normal operation the optimum engine/rotor spe

Plaster molds, Plastic molds are made of plaster of Paris (gypsum) or calci...

Plastic molds are made of plaster of Paris (gypsum) or calcium sulphate, talc and silica flour is added in the plaster of Paris to improve strength and to control the time required

Noise suppression in aircraft design, Noise Suppression in Aircraft Design:...

Noise Suppression in Aircraft Design: It has been seen that the first step towards noise suppression is at the design stage of the rotating and static parts of the engine. The

Hot and cold working, the amount of cold working metal can withstand is dir...

the amount of cold working metal can withstand is directly related to which properties? name two and also discuss the effect that cold working has upon these properties?

machine molding, Machine molding is suitable for the faster and uniform qu...

Machine molding is suitable for the faster and uniform quality moulds, needed for mass production of castings. For preparing the moulds, various moulding machines are used. Majorit

Aerofoil theory and the axial flow compressor, Aerofoil theory and the axia...

Aerofoil theory and the axial flow compressor  The blades of the axial flow compressor are aerofoils and as such behave in a similar way to aircraft mainplanes and propeller bl

Oil pumps - aircraft engine, OIL PUMPS The oil pumps fitted in a recirc...

OIL PUMPS The oil pumps fitted in a recirculatory system are normally gear-type or Gerotor type pumps. The pumps are usually mounted in a pack containing one pressure pump and

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