experiment.asv

%% MA342 Project 1
%% Experiment 1 - Increasing the number of panels
clear variables;
close all;
clc;

v = 76;         % m/s
naca2418 = importdata('naca2418.dat.txt');
naca64209 = importdata('naca64209.dat.txt');
fx84w097 = importdata('fx84w097.dat.txt');
mh112 = importdata('mh112.dat.txt');

data = {};
data{1} = 

num_panels = transpose(5:2:35);

figure;

for d = 1:length(data_exp)
    C_L1 = zeros(length(num_panels), 1);

    for i = 1:length(C_L1)
        X = points_based_on_input(data_exp(d),num_panels(i));
        X = [X; X(1, :)];
        X = [X; [1.1, -0.05]];
        C_L1(i) = airfoil_wing(X, v, false);
    end

    plot(num_panels, C_L1);
end

grid on;
title("Experiment 1: Altering the number of panels")
xlabel("Number of Panels");
ylabel("Lift Coefficient (C_L)");

%% Experiment 2 - Changing the wake angle
wa_length = 0.1118;
theta_max = pi/4;
theta_iter = linspace(0, theta_max, 25);
num_panels_2 = 13;

figure;

for d = 1:length(data_exp)
    C_L2 = zeros(length(theta_iter), 1);
    for i = 1:length(C_L2)
        X = points_based_on_input(naca2418, num_panels_2);
        X = [X; X(1, :)];
        X = [X; [1 + wa_length*cos(theta_iter(i)), -wa_length*sin(theta_iter(i))]];
        C_L2(i) = airfoil_wing(X, v, false);
    end

    plot(theta_iter, C_L2);
end

grid on;
title("Experiment 2: Altering the wake angle")
xlabel("Wake Angle Theta (rad)");
ylabel("Lift Coefficient (C_L)");