RCAIDE.Library.Plots.Aerodynamics

Aerodynamics

RCAIDE Aerodynamics Plotting Package

This package contains modules for visualizing aerodynamic analysis results and performance characteristics.

See also

RCAIDE.Library.Plots

Parent plotting package

RCAIDE.Library.Methods.Aerodynamics

Aerodynamic analysis tools

Modules

plot_aerodynamic_coefficients(results[, ...])	Creates a multi-panel visualization of aerodynamic coefficients throughout flight.
plot_aerodynamic_forces(results[, ...])	Creates a multi-panel visualization of aerodynamic forces throughout flight.
plot_aircraft_aerodynamics(results[, ...])	Creates 3D surface plots of aircraft lift and drag coefficients as functions of Mach number and angle of attack.
plot_airfoil_boundary_layer_properties(ap[, ...])	Generate plots of airfoil boundary layer properties and distributions.
plot_airfoil_polar_files(polar_data[, ...])	Generate plots of airfoil performance data from polar files.
plot_airfoil_polars(polar_data[, ...])	Generate plots of airfoil aerodynamic characteristics from analysis results.
plot_airfoil_surface_forces(ap[, ...])	Generate plots showing pressure forces on airfoil surface using arrows.
plot_disc_and_power_loading(results[, ...])	Generate plots of rotor disc and power loading over time.
plot_drag_components(results[, save_figure, ...])	Generate plots showing the breakdown of aircraft drag components over time.
plot_lift_distribution(results[, ...])	Generate plots of spanwise lift distribution for lifting surfaces.
plot_rotor_conditions(results[, ...])	Generate plots of key rotor operating conditions over time.
plot_rotor_disc_performance(prop, outputs[, ...])	Generate plots of rotor disc aerodynamic performance distributions.
plot_rotor_performance(rotor, outputs[, ...])	Generate plots summarizing rotor aerodynamic performance distributions.
plot_surface_pressures(results[, ...])	Creates contour plots of surface pressure distributions on aircraft lifting surfaces.