fvw_types::fvw_initinputtype Type Reference

Collaboration diagram for fvw_types::fvw_initinputtype:

Public Attributes
character(1024)	fvwfilename
	Main FVW input file name [-].
character(1024)	rootname
	RootName for writing output files [-].
type(wng_initinputtype), dimension(:), allocatable	w
	Number of blades [-].
type(meshtype), dimension(:), allocatable	wingsmesh
	Input Mesh defining position and orientation of wings (nSpan+1) [-].
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]
logical	sumprint
	Whether to print summary file (primarially in in UA) [-].

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

• FVW_Types.f90