protected class NACA4Uncambered.Ordinate
extends java.lang.Object
Modifier and Type | Field and Description |
---|---|
double |
tanth
The tangent of the local surface angle due to camber.
|
double |
thp
The local surface angle due to camber.
|
double |
y
Ordinate (Y coordinate) of the uncambered airfoil.
|
double |
yCMB
The offset in the ordinate from the uncambered airfoil
to the cambered airfoil.
|
double |
yp
The local slope of the uncambered airfoil: yp = dy/dx.
|
double |
ypp
The rate of change of the local slope of the
uncambered airfoil: ypp = dy^2/dx^2.
|
Modifier | Constructor and Description |
---|---|
protected |
NACA4Uncambered.Ordinate() |
public double y
public double yp
public double ypp
public double yCMB
public double tanth
public double thp