fvw_types::fvw_initinputtype Type Reference

Public Attributes
character(1024)	fvwfilename
	Main FVW input file name [-].
character(1024)	rootname
	RootName for writing output files [-].
type(meshtype), dimension(:), allocatable	wingsmesh
	Input Mesh defining position and orientation of wings (nSpan+1) [-].
integer(intki), dimension(:,:), allocatable	afindx
	Index to the airfoils from AD15 [idx1=BladeNode, idx2=Blade number] [-].
real(reki), dimension(:,:), allocatable	chord
	Chord of each blade element from input file [idx1=BladeNode, idx2=Blade number] [-].
real(reki), dimension(:), allocatable	relm
	radius of center of each element [-]
real(reki), dimension(:), allocatable	zhub
	Distance to hub for each blade [m].
real(reki), dimension(:,:), allocatable	zlocal
	Distance to blade node, measured along the blade [m].
real(reki), dimension(:), allocatable	ztip
	Distance to blade tip, measured along the blade [m].
real(reki), dimension(:,:), allocatable	rlocal
	Radial distance to blade node from the center of rotation, measured in the rotor plane, needed for DBEMT [m].
integer(intki)	numblades
	Number of blades [-].
integer(intki)	numbladenodes
	Number of nodes on each blade [-].
real(dbki)	dtaero
	Time interval for calls (from AD15) [s].
real(reki)	kinvisc
	Kinematic air viscosity [m^2/s].
integer(intki)	uamod
	Model for the dynamic stall equations [1 = Leishman/Beddoes, 2 = Gonzalez, 3 = Minnema] [-].
logical	ua_flag
	logical flag indicating whether to use UnsteadyAero [-]
logical	flookup
	Use table lookup for f' and f'' [-].
real(reki)	a_s
	speed of sound [m/s]

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

• FVW_Types.f90