[][src]Struct rs_xfoil::Config

pub struct Config { /* fields omitted */ }

Struct tracking Xfoil configuration.

Methods

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

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

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.

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.

Set path of polar file to save Xfoil data into.

Specify a 4-digit NACA airfoil code.

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

Set a Reynolds number for a viscous calculation.

Auto Trait Implementations

impl Send for Config

impl Sync for Config

Blanket Implementations

impl<T, U> Into for T where
    U: From<T>, 
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impl<T> From for T
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impl<T, U> TryFrom for T where
    T: From<U>, 
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🔬 This is a nightly-only experimental API. (try_from)

The type returned in the event of a conversion error.

impl<T> Borrow for T where
    T: ?Sized
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impl<T> Any for T where
    T: 'static + ?Sized
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impl<T> BorrowMut for T where
    T: ?Sized
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impl<T, U> TryInto for T where
    U: TryFrom<T>, 
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🔬 This is a nightly-only experimental API. (try_from)

The type returned in the event of a conversion error.