Ejemplo n.º 1
0
 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");
 }
Ejemplo n.º 2
0
        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);
        }
Ejemplo n.º 3
0
        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");
 }