class Rotor

Basic Rotor class (development release)

Public Methods

[more] Rotor()
[more] ~Rotor()
[more]void CalcDepVars()
[more]void ComputeCT_and_vi()
Compute the values of the dependent variables

Public Members

class Rotor_NewtonMethod: public Newton<Rotor>

Private Fields

[more]int b
Geometry variables
[more]double R
number of blades
[more]double c
radius (m)
[more]double theta1
mean chord of blades (m)
[more]Vector3D r_hub
blade torsion ()
[more]double Izz
Inertia/Mechanics
[more]double a
Aerodynamic variables
[more]double delta_0
mean lift coefficient of blades (1/rad)
[more]double delta_1
[more]double delta_2
[more]double B
Coefficients of drag: cd=delta0+delta1*alpha+delta2*alpha^2
[more]double k_i
Modified Momentum Theory constants:
[more]double k_v
[more]double eta_w
[more]double omega
State variables
[more]double omega_nom
rotor spin velocity (rad/seg)
[more]Vector3D velocity
nominal rotor spin velocity.
[more]double rho
velocity respect to air in global axes
[more]double sigma
Computed variables --------------------------------------------------------
[more]double lock
solidity
[more]double v_i
Intermediate variables:
[more]double lambda_i
induced velocity
[more]double mu
non-dimensional induced velocity (1/omega R)?
[more]double mu_z
advance parameter
[more]double theta_C
Control variables
[more]double CT
Non-dimensional Forces and Moments;
[more]double CQ
Thrust coefficient


Documentation

Basic Rotor class (development release)
o Rotor()

o ~Rotor()

ovoid CalcDepVars()

ovoid ComputeCT_and_vi()
Compute the values of the dependent variables

oint b
Geometry variables

odouble R
number of blades

odouble c
radius (m)

odouble theta1
mean chord of blades (m)

oVector3D r_hub
blade torsion ()

odouble Izz
Inertia/Mechanics

odouble a
Aerodynamic variables

odouble delta_0
mean lift coefficient of blades (1/rad)

odouble delta_1

odouble delta_2

odouble B
Coefficients of drag: cd=delta0+delta1*alpha+delta2*alpha^2

odouble k_i
Modified Momentum Theory constants:

odouble k_v

odouble eta_w

odouble omega
State variables

odouble omega_nom
rotor spin velocity (rad/seg)

oVector3D velocity
nominal rotor spin velocity. (rad/seg)

odouble rho
velocity respect to air in global axes

odouble sigma
Computed variables --------------------------------------------------------

odouble lock
solidity

odouble v_i
Intermediate variables:

odouble lambda_i
induced velocity

odouble mu
non-dimensional induced velocity (1/omega R)?

odouble mu_z
advance parameter

odouble theta_C
Control variables

odouble CT
Non-dimensional Forces and Moments;

odouble CQ
Thrust coefficient


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