125 static double DragCoefficient(
double liftCoefficient,
double cd0,
double aspectRatio,
double oswald);
The symmetric-foil coefficient model. All members are static and pure.
Definition AuvFoil.h:92
static AuvFoilCoefficients Coefficients(double alpha, const AuvFoilProperties &foil)
static double LiftCoefficient(double alpha, double clMax, double aoaMax)
static double LiftCoefficientSlope(double alpha, double clMax, double aoaMax)
static double DragCoefficient(double liftCoefficient, double cd0, double aspectRatio, double oswald)
double liftSlope
, per radian.
Definition AuvFoil.h:72
double dragSlope
, per radian.
Definition AuvFoil.h:73
double lift
, dimensionless.
Definition AuvFoil.h:70
double drag
, dimensionless.
Definition AuvFoil.h:71
double aoaMax
Angle of attack of peak lift, rad (25 degrees).
Definition AuvFoil.h:84
double oswald
Oswald span efficiency of the induced drag term.
Definition AuvFoil.h:87
double aspectRatio
Fin aspect ratio, span squared over area.
Definition AuvFoil.h:86
double clMax
Peak lift coefficient, reached at aoaMax.
Definition AuvFoil.h:83
double cd0
Profile drag coefficient at zero lift.
Definition AuvFoil.h:85