airfoilinfo_types::afi_outputtype Type Reference

Public Attributes
real(reki)	cl = 0.
	Dimensionless coefficient of lift [-].
real(reki)	cd = 0.
	Dimensionless coefficient of drag [-].
real(reki)	cm = 0.
	Dimensionless coefficient of pitching moment [-].
real(reki)	cpmin = 0.
	Dimensionless coefficient of minimum pressure [-].
real(reki)	cd0 = 0.
	Minimum Cd value (used for Beddoes-Leishman unsteady aero) [-].
real(reki)	cm0 = 0.
	2D pitching moment coefficient at zero lift, positive if nose is up [-]
real(reki)	f_st = 0.
	separation function based on cl or cn (used for UA models) [-]
real(reki)	fullyseparate = 0.
	fully separated cn or cl polar function (used for UA models) [-]
real(reki)	fullyattached = 0.
	fully attached cn or cl polar function (used for UA models) [-]

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

• AirfoilInfo_Types.f90