Expand description
Re-exports§
pub use atmosphere::dynamic_pressure;pub use atmosphere::mach_number;pub use atmosphere::speed_of_sound;pub use atmosphere::standard_density;pub use atmosphere::standard_pressure;pub use atmosphere::standard_temperature;pub use coefficients::drag_coefficient;pub use coefficients::lift_coefficient_thin_airfoil;pub use error::PavanError;pub use error::Result;pub use forces::AeroForce;pub use forces::body_to_wind;pub use forces::drag;pub use forces::lift;pub use forces::reynolds_number;pub use airfoil::NacaProfile;pub use airfoil::SurfacePoints;pub use panel::Panel;pub use panel::PanelSolution;pub use vehicle::AeroBody;pub use vlm::VlmSolution;pub use vlm::WingGeometry;pub use wind::WindField;
Modules§
- airfoil
- atmosphere
- boundary
- coefficients
- compressible
- Compressible flow relations for gasdynamics.
- error
- forces
- panel
- Hess-Smith 2D panel method for potential flow around airfoils.
- propulsion
- Propulsion models for thrust, fuel consumption, and efficiency.
- stability
- Longitudinal static stability, control surfaces, and trim.
- vehicle
- vlm
- Vortex Lattice Method (VLM) for 3D finite wings.
- wind