public Gear(Aerodata a):base(a)
{
MaxSteer = new DenominatedAmount(0, "DEG");
dynamic_friction = new DenominatedAmount(0.5,null);
rolling_friction = new DenominatedAmount(0.02,null);
static_friction = new DenominatedAmount(0.8, null);
spring_coeff = new DenominatedAmount(a.EmptyWeight.Amount * 0.9, "LBS/FT");
damping_coeff = new DenominatedAmount(a.EmptyWeight.Amount * 0.05, "LBS/FT/SEC");
}
public Tank(string name, double p1, double p2, double p3, string units, int pri, int capacity,string fuel_units, double? standpipe )
{
Name = name;
Priority = pri;
Location = new Location(p1, p2, p3, units);
Capacity = new DenominatedAmount(capacity, fuel_units);
if (standpipe.HasValue)
Standpipe = new DenominatedAmount(standpipe.Value, fuel_units);
}
internal Location FromChord(DenominatedAmount chord, double percentX, double percentY, double percentZ )
{
if (percentX > 1) percentX /= 100;
if (percentY > 1) percentY /= 100;
if (percentY > 1) percentZ /= 100;
if (chord.Unit != Unit)
throw new Exception("Must be in same units");
return new Location(percentX * chord.Amount + X,
percentY * chord.Amount + Y,
percentZ * chord.Amount + Z,
Unit);
}
public GroundReactionElement(Aerodata a)
{
spring_coeff = a.EmptyWeight;
spring_coeff = new DenominatedAmount(a.EmptyWeight.Amount * 0.9, "LBS/FT");
damping_coeff = new DenominatedAmount(a.EmptyWeight.Amount * 0.2, "LBS/FT/SEC");
}
