NAME						UNITS					VARIABLE		VALUE
Rotor Radius 					(meters)				R		=	0.6096	 
Initial Pitch Angle 				(degrees)				theta		=	-10		
Pitch Angle Flap Coupling 			(degrees) 				delta_3		=	-41		
Flap Angle 					(degrees) 				beta		=	-4		
Precone Angle 					(degrees) 				beta_p		=	-4		
Initial Angle of Attack 			(degrees) 				alpha		=	-90		
Rotations per Minute 				(rpm)					RPM		=	0		
Twist Rate 					(degrees/meter)				theta_tw	=	15.2
Blade Chord 					(meters) 				c 		=	0.0762
Number of Blade Elements 			(unitless) 				n		=	10
Number of Blades 				(unitless) 				N_b		=	4
Mass of the Model 				(kilograms) 				m_total		=	2.26796
Mass of The Blade 				(kilograms) 				m_blade		=	0.0846
The Hinge Offset 				(meters) 				e		=	0.01
The Flapping Stiffness 				(Newton meter per radian) 		k_beta		=	313
Blade Width 		     			(meters) 				y		=	0.015

AirFoil 					(unitless)				AirFoil		=	SC1095

Starting Time                                   (seconds)				time            =       0
Time Step                                       (seconds)				timeStep        =       15
Altitude 					(meters) 				A		=	30000