Question

The pressure coefficient distribution around a slender body of chord ? = 1 is given by ??? = −3 (1 − ? ?) ??? = (1 − ? ?). Where x goes from zero to ?.

Create a MATLAB algorithm that calculates the total lift coefficient acting on the body and plot the pressure coefficient distribution (inverting the y-axis, to display ??? above the x-axis).

*Use at least 100 points

**attach your plot, with the total lift coefficient as a TITLE in the plot. Also attach a copy of your “well commented” code

Answer 1

`Hey,

Note: Brother if you have any queries related the answer please do comment. I would be very happy to resolve all your queries.

clc
clear all
close all
format long
c=1;
x=linspace(0,c,1000);
cpu=-3*(1-x.^c);
cpl=(1-x.^c);
plot(cpu,cpl);
xlabel('cpu');
ylabel('cpl');
title('Plot of cpu vs cpl');

Kindly revert for any queries

Thanks.