commence class-ification of gui

1 files changed, 35 insertions, 0 deletions

diff --git a/wing_scripts/get_int.m b/wing_scripts/get_int.m
new file mode 100644
index 0000000..edbfda3
--- /dev/null
+++ b/wing_scripts/get_int.m
@@ -0,0 +1,35 @@
+function z = get_int(xi,xf,u)
+
+M = 0.02;
+P = 0.4;
+T = 0.12;
+a0 = 0.2969;
+a1 = -0.126;
+a2 = -0.3516;
+a3 = 0.2843;
+a4 = -0.1015;
+
+
+%evaluate the integral of camber line, depending on xi and xf related to P
+
+if xf <P
+    intCamb =  M/P^2*(2*P*xf^2/2 - xf^3/3) - M/P^2*(2*P*xi^2/2 - xi^3/3);   
+elseif xi<P
+    intCamb = (M/(1-P)^2)*((1 - 2*P)*xf +2*P*xf^2/2 - xf^3/3) - (M/(1-P)^2)*((1 - 2*P)*P +2*P*P^2/2 - P^3/3);
+    intCamb = intCamb + M/P^2*(2*P*P^2/2 - P^3/3) - M/P^2*(2*P*xi^2/2 - xi^3/3);
+else
+    intCamb = (M/(1-P)^2)*((1 - 2*P)*xf +2*P*xf^2/2 - xf^3/3) - (M/(1-P)^2)*((1 - 2*P)*xi +2*P*xi^2/2 - xi^3/3);
+end
+
+% do integral on thickness line
+%z_thickness = (T/0.2)*(a0*x^.5+a1*x+a2*x^2+a3*x^3+a4*x^4);
+
+intThickness = (T/0.2)*(a0*xf^1.5/1.5 + a1*xf^2/2 + a2*xf^3/3 + a3*xf^4/4 +a4*xf^5/5);
+intThickness = intThickness - (T/0.2)*(a0*xi^1.5/1.5 + a1*xi^2/2 + a2*xi^3/3 + a3*xi^4/4 +a4*xi^5/5);
+
+% combine both integral results to get total integral
+if u == 1
+   z = intCamb + intThickness; 
+else
+   z = abs(intCamb - intThickness);
+end
\ No newline at end of file