m_derived_types::ib_airfoil_parameters Type Reference

User-input parameters for a NACA 4-digit airfoil (namelist-safe: scalars only). More...

Public Attributes
real(wp)	c = dflt_real
	chord length
real(wp)	p = dflt_real
	maximum camber position (fraction of chord)
real(wp)	t = dflt_real
	maximum thickness (fraction of chord)
real(wp)	m = dflt_real
	maximum camber (fraction of chord)

Detailed Description

User-input parameters for a NACA 4-digit airfoil (namelist-safe: scalars only).

Definition at line 582 of file m_derived_types.fpp.f90.

Member Data Documentation

c

real(wp) m_derived_types::ib_airfoil_parameters::c = dflt_real

chord length

Definition at line 583 of file m_derived_types.fpp.f90.

m

real(wp) m_derived_types::ib_airfoil_parameters::m = dflt_real

maximum camber (fraction of chord)

Definition at line 586 of file m_derived_types.fpp.f90.

p

real(wp) m_derived_types::ib_airfoil_parameters::p = dflt_real

maximum camber position (fraction of chord)

Definition at line 584 of file m_derived_types.fpp.f90.

t

real(wp) m_derived_types::ib_airfoil_parameters::t = dflt_real

maximum thickness (fraction of chord)

Definition at line 585 of file m_derived_types.fpp.f90.

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

• m_derived_types.fpp.f90