Struct AeroBody 

#[non_exhaustive]
pub struct AeroBody {
    pub reference_area: f64,
    pub cd0: f64,
    pub aspect_ratio: f64,
    pub oswald_efficiency: f64,
    pub chord: f64,
}

An aerodynamic body with reference properties.

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.

reference_area: f64

Reference area (m²) — typically wing area for aircraft.

cd0: f64

Zero-lift drag coefficient.

aspect_ratio: f64

Wing aspect ratio (span² / area).

oswald_efficiency: f64

Oswald efficiency factor (0.7–0.85 typical).

chord: f64

Chord length (m) — for moment computation.

Implementations

impl AeroBody

pub fn light_aircraft() -> Self

Typical light aircraft (Cessna 172 class).

pub fn glider() -> Self

High-performance glider.

pub fn compute_forces( &self, velocity: f64, altitude: f64, angle_of_attack_rad: f64, ) -> AeroForce

Compute aerodynamic forces at given conditions.

Trait Implementations

impl Clone for AeroBody

fn clone(&self) -> AeroBody

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Debug for AeroBody

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

Formats the value using the given formatter.

impl<'de> Deserialize<'de> for AeroBody

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

where __D: Deserializer<'de>,

Deserialize this value from the given Serde deserializer.

impl Serialize for AeroBody

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

where __S: Serializer,

Serialize this value into the given Serde serializer.