Struct lib::Config

pub struct Config { /* fields omitted */ }

Struct tracking Xfoil configuration.

Methods

impl Config

pub fn new(path: &str) -> Self

Create new Xfoil configuration structure from the path to an Xfoil executable.

pub fn get_runner(self) -> Result<XfoilRunner>

Construct XfoilRunner from configuration panics: if no airfoil (either from polar file or NACA code) is given.

pub fn angle_of_attack(self, angle: f64) -> Self

Set angle of attack at which to run xfoil computation. If lift_coefficient was previously called, the state is overwritten to use an angle of attack calculation instead.

pub fn lift_coefficient(self, cl: f64) -> Self

Set lift coefficient at which to run xfoil computation. If angle_of_attack was previously called, the state is overwritten to use a lift coefficient calculation instead.

pub fn polar_accumulation(self, fname: &str) -> Self

Set path of polar file to save Xfoil data into.

pub fn naca(self, code: &str) -> Self

Specify a 4-digit NACA airfoil code.

pub fn airfoil_polar_file(self, path: &str) -> Self

Specify a file containing airfoil coordinates to use in Xfoil computation.

pub fn reynolds(self, reynolds: usize) -> Self

Set a Reynolds number for a viscous calculation.