Collaboration diagram for aerodyn_types::rotinputfile:

Public Attributes
type(ad_bladepropstype), dimension(:), allocatable	bladeprops
	blade property information from blade input files [-]

integer(intki)	numtwrnds
	Number of tower nodes used in the analysis [-].

real(reki), dimension(:), allocatable	twrelev
	Elevation at tower node [m].

real(reki), dimension(:), allocatable	twrdiam
	Diameter of tower at node [m].

real(reki), dimension(:), allocatable	twrcd
	Coefficient of drag at tower node [-].

real(reki), dimension(:), allocatable	twrti
	Turbulence intensity for tower shadow at tower node [-].

real(reki), dimension(:), allocatable	twrcb
	Coefficient of buoyancy at tower node [-].

real(reki)	volhub
	Hub volume [m^3].

real(reki)	hubcenbx
	Hub center of buoyancy x direction offset [m].

real(reki)	volnac
	Nacelle volume [m^3].

real(reki), dimension(1:3)	naccenb
	Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates [m].

logical	tfinaero = .FALSE.
	Calculate tail fin aerodynamics model (flag) [flag].

character(1024)	tfinfile
	Input file for tail fin aerodynamics [used only when TFinAero=True] [-].

type(tfininputfiletype)	tfin
	Input file data for tail fin [-].

The documentation for this type was generated from the following file:

Public Attributes