blob: cbea2aa35dadae923dc49dd7b5d93f3b1633d6e1 (
plain)
1
2
3
4
5
6
7
8
|
//for the CP-1:
W=13127.5;//normal gross weight(N)
S=16.165;//wingarea(m^2)
a=4.2*%pi/180;//approx minimum glide angle(radian).from example 6.7
D1=0.905;//density at 3048 m(Kg/m^3)
D2=1.155;//density at 609.6 m(Kg/m^3)
Cl=0.634;//lift coefficient corresponding to minimum glide angle i.e maximum L/D(from example 6.1)
Wl=W/S//wing loading (W/S in N/m^2)
|
