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(Solved) Problem 1 Using Excel create a graph of the following theoretical function for Lift of an airplane (Lift vs. Velocity) for 2 lift coefficients CL....


Please help, it would be nice if it could get done tonight!!

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Problem 1
Using Excel create a graph of the following theoretical function for Lift of an airplane (Lift vs. Velocity)
for 2 lift coefficients CL. 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. 1
L = ECLpVZS
Where:
L = Lift (lb)
CL = Lift Coefficient (unitless), use 0.30 and 0.52 for this graph
p = Density ofthe air, we will use the density at 40,000 ft, p = 000058735 1% V = Velocity of the airplane (ft/s)
S =Area ofthe wings, S = 5500 ft2 Problem 2 Complete the same problem as above in MATLAB. Note, you cannotjust copy and paste the values in
from Excel. You must create the vectors inside your MATLAB script file.

 


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