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

Lifting wing, Lifting wing FP was run at the conditions corresponding t...

Lifting wing FP was run at the conditions corresponding to AGARD WG07 TEST CASE 11, namely M∞ = 0.84,α= 3.06 deg. The ‘final step' values of the partially-conservative paramete

Civil engg projects, wat r d new transportation based projects for d civil ...

wat r d new transportation based projects for d civil engg. students..??

thermoelectric effect, Thermoelectric effect The measurement of temper...

Thermoelectric effect The measurement of temperature using a thermocouple relies on Seebeck effect. The electrons occupy different energy levels in different materials

Heat capacity, Specific heat capacity of water in a continues flow method?

Specific heat capacity of water in a continues flow method?

Payback period method, Non-discounted cash flow method, Payback period met...

Non-discounted cash flow method, Payback period method In this method, time value of money is not considered. It takes into account the number of years required to recover the in

Industrial engineering programmes, "Whether you are writing, listening, spe...

"Whether you are writing, listening, speaking, or attending meetings, communication skills are critical to your success in University and the workplace". Discuss. Since entering

Aviation legislation - certificate of design, Aviation legislation - Certif...

Aviation legislation - Certificate of Design: During the construction, the manufacturer has to provide the C.A.A. with a Certificate of Design and also a Type Record for th

Pressure relief valve - aircraft engine, PRESSURE RELIEF VALVE The pres...

PRESSURE RELIEF VALVE The pressure relief valve shown in the figure. controls the oil pressure at the pre-set value demanded by the system. The valve is normally integral with

Pn junction diode, what is the effect of temperature on pn junction diode o...

what is the effect of temperature on pn junction diode of component

Polymorphism, Q.  Define the polymorphism. Ans. POLYMORPHISM: It is d...

Q.  Define the polymorphism. Ans. POLYMORPHISM: It is defined as the change in atomic structure which occurs at a definite transformation temperature. The cooling diagram of

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