Academic Integrity: tutoring, explanations, and feedback — we don’t complete graded work or submit on a student’s behalf.

This is a matlab programming assignment.Thanks! Using Excel create a graph of th

ID: 3819286 • Letter: T

Question

This is a matlab programming assignment.Thanks!

Using Excel create a graph of the following theoretical function tor Lift of an airplane (Lift vs. Velocity) for 2 lift coefficients C_L. Create your Excel sheet so you are using absolute references for the constants. Your Velocity (x values) should range from 300 ft/s to 700 ft/s. You must choose an appropriate step size to create a smooth plot. Use good graphing practices. L = 1/2 C_L rho V^2 S Where: L = Lift (lb) C_L = Lift Coefficient (unit less), use 0.30 and 0.52 for this graph rho = Density of the air, we will use the density at 40,000 ft, rho = 0.00058735 slug/ft^2 V = Velocity of the airplane (ft/s) S = Area of the wings, S = 5500 ft^2 Complete the same problem as above in MATLAB. Note, you cannot just copy and paste the values in from Excel. You must create the vectors inside your MATLAB script file. A concept map is used to visualize the relationships between different topics and concepts. It includes concepts connected with lines. The lines of a concept map include words to describe the relationship of the 2 connected items. Here is an example of a concept map for the seasons. http://cmap.ihmc.us/docs/images/Theory/Fig5CmapSeasons-large.png You are to create a concept map for ENGR 1181. This can be created by hand or on the computer, however it is to be submitted via Carmen. You can use the internet to look up additional examples of concept maps. Use this problem to identify areas to study for the Final Exam.

Explanation / Answer

syms f Cl V p S
f=0.5*Cl*p*(V^(2))*S
subs(f,[Cl,V,p,S],[0.30,300,0.00058735,5500])
%Cl=[0.30:0.52];
%p=0.00058735;
%V=[300:700];
%S=5500;
subs(f,{Cl,V},[0.30 700])
grid on;

Hire Me For All Your Tutoring Needs
Integrity-first tutoring: clear explanations, guidance, and feedback.
Drop an Email at
drjack9650@gmail.com
Chat Now And Get Quote