Struct WingGeometry 

#[non_exhaustive]
pub struct WingGeometry {
    pub span: f64,
    pub root_chord: f64,
    pub tip_chord: f64,
    pub sweep_le_rad: f64,
    pub dihedral_rad: f64,
    pub twist_tip_rad: f64,
    pub n_span: usize,
    pub n_chord: usize,
}

Wing planform definition for VLM analysis.

Fields (Non-exhaustive)

Non-exhaustive structs could have additional fields added in future. Therefore, non-exhaustive structs cannot be constructed in external crates using the traditional Struct { .. } syntax; cannot be matched against without a wildcard ..; and struct update syntax will not work.

span: f64

Full wingspan (m), tip to tip.

root_chord: f64

Root chord length (m).

tip_chord: f64

Tip chord length (m). Equal to root_chord for rectangular wings.

sweep_le_rad: f64

Leading edge sweep angle (rad). 0 for unswept.

dihedral_rad: f64

Dihedral angle (rad). 0 for flat wing.

twist_tip_rad: f64

Geometric twist at tip relative to root (rad). Negative = washout.

n_span: usize

Spanwise panels per semi-span.

n_chord: usize

Chordwise panels.

Implementations

impl WingGeometry

pub fn rectangular(span: f64, chord: f64, n_span: usize, n_chord: usize) -> Self

Rectangular wing (no taper, no sweep, no twist).

pub fn tapered( span: f64, root_chord: f64, tip_chord: f64, n_span: usize, n_chord: usize, ) -> Self

Tapered wing (no sweep, no twist).

pub fn reference_area(&self) -> f64

Wing reference area: S = span × (root + tip) / 2.

pub fn aspect_ratio(&self) -> f64

Aspect ratio: AR = span² / S.

pub fn total_panels(&self) -> usize

Total number of panels (both semi-spans × chordwise).

Trait Implementations

impl Clone for WingGeometry

fn clone(&self) -> WingGeometry

Returns a duplicate of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Debug for WingGeometry

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.

impl<'de> Deserialize<'de> for WingGeometry

fn deserialize<__D>(__deserializer: __D) -> Result<Self, __D::Error>

where __D: Deserializer<'de>,

Deserialize this value from the given Serde deserializer.

impl Serialize for WingGeometry

fn serialize<__S>(&self, __serializer: __S) -> Result<__S::Ok, __S::Error>

where __S: Serializer,

Serialize this value into the given Serde serializer.