// Create a propeller branch 1 of dual engine system
// Number of branches: 	1
// Number of masses:	13
// Components: Propeller

// Create inertias
dataModel.Add(M37 = new Inertia() { X=601; Y=172; Description="M37" });
dataModel.Add(M38 = new Inertia() { X=676; Y=172; Description="M38" });
dataModel.Add(M39 = new Inertia() { X=706; Y=172; Description="M39" });
dataModel.Add(M40 = new Inertia() { X=736; Y=172; Description="M40" });
dataModel.Add(M41 = new Inertia() { X=766; Y=172; Description="M41" });
dataModel.Add(M42 = new Inertia() { X=796; Y=172; Description="M42" });
dataModel.Add(M43 = new Inertia() { X=826; Y=172; Description="M43" });
dataModel.Add(M44 = new Inertia() { X=856; Y=172; Description="M44" });
dataModel.Add(M45 = new Inertia() { X=886; Y=172; Description="M45" });
dataModel.Add(M46 = new Inertia() { X=906; Y=172; Description="M46" });
dataModel.Add(M47 = new Inertia() { X=936; Y=172; Description="M47" });
dataModel.Add(M48 = new Inertia() { X=966; Y=172; Description="M48" });
dataModel.Add(M49 = new Propeller() { X=1006; Y=172; Description="M49" });

// Add stiffness
dataModel.Add(Mesh1 = new Mesh(M18, M37));
dataModel.Add(Mesh2 = new Mesh(M36, M37));
dataModel.Add(S37 = new Stiffness(M37, M38));
dataModel.Add(S38 = new Stiffness(M38, M39));
dataModel.Add(S39 = new Stiffness(M39, M40));
dataModel.Add(S40 = new Stiffness(M40, M41));
dataModel.Add(S41 = new Stiffness(M41, M42));
dataModel.Add(S42 = new Stiffness(M42, M43));
dataModel.Add(S43 = new Stiffness(M43, M44));
dataModel.Add(S44 = new Stiffness(M44, M45));
dataModel.Add(S45 = new Stiffness(M45, M46));
dataModel.Add(S46 = new Stiffness(M46, M47));
dataModel.Add(S47 = new Stiffness(M47, M48));
dataModel.Add(S48 = new Stiffness(M48, M49));

// Group into gear
Gear1 = new Gear();
Gear1.Add(M18);
Gear1.Add(M36);
Gear1.Add(M37);
dataModel.Add(Gear1);

// Mass properties
M37.MomentOfInertia = 10920 kg*m^2;
M38.MomentOfInertia = 56.18 kg*m^2;
M39.MomentOfInertia = 161 kg*m^2;
M40.MomentOfInertia = 156.1 kg*m^2;
M41.MomentOfInertia = 28.72 kg*m^2;
M42.MomentOfInertia = 108.8 kg*m^2;
M43.MomentOfInertia = 181.2 kg*m^2;
M44.MomentOfInertia = 37.19 kg*m^2;
M45.MomentOfInertia = 35.91 kg*m^2;
M46.MomentOfInertia = 410.5 kg*m^2;
M47.MomentOfInertia = 483.7 kg*m^2;
M48.MomentOfInertia = 208.8 kg*m^2;
M49.InertiaInAir = 32460 kg*m^2;
M49.InertiaOfEntrainedWater = 0 kg*m^2;


// Stiffness properties
Mesh1.TorsionalStiffness = 1000000000 N*m/rad;
Mesh2.TorsionalStiffness = 1000000000 N*m/rad;
S37.TorsionalStiffness = 293100000 N*m/rad;
S38.TorsionalStiffness = 342700000 N*m/rad;
S39.TorsionalStiffness = 77900000 N*m/rad;
S40.TorsionalStiffness = 384500000 N*m/rad;
S41.TorsionalStiffness = 384600000 N*m/rad;
S42.TorsionalStiffness = 121300000 N*m/rad;
S43.TorsionalStiffness = 112500000 N*m/rad;
S44.TorsionalStiffness = 332600000 N*m/rad;
S45.TorsionalStiffness = 399900000 N*m/rad;
S46.TorsionalStiffness = 112400000 N*m/rad;
S47.TorsionalStiffness = 48930000 N*m/rad;
S48.TorsionalStiffness = 374300000 N*m/rad;

// Propeller properties
M49.PowerMCR = 12400 kW;
M49.SpeedMCR = 137.8 rpm;
M49.BladeNumber = 5;
M49.DampingModel = "Manual";
M49.FirstOrderTorqueAmplitude = 0.07;
M49.SecondOrderTorqueAmplitude = 0.02;
