public Stabilizer LoadDefaultVertical()
{
airfoil = Airfoil.Get("NACA0012");
span = 2.0;
chord = 0.7;
return(this);
}
public Stabilizer LoadDefaultHorizontal()
{
airfoil = Airfoil.Get("NACA0012");
span = 3.2;
chord = 0.4;
return(this);
}
public void TestAirfoil()
{
Airfoil airfoil = Airfoil.Get("NACA0012");
Assert.AreEqual(0.755, airfoil.CL(-165), 0.01);
Assert.AreEqual(0.256, airfoil.CD(-165), 0.01);
Assert.AreEqual(0.326, airfoil.CM(-165), 0.01);
}
public static void Add(Airfoil airfoil)
{
airfoils[airfoil.name] = airfoil;
}
