Source code for aerosandbox.library.regulations.far_part_23

import aerosandbox.numpy as np
from aerosandbox.tools import units as u
from typing import Tuple


### See also:
# https://www.risingup.com/fars/info/23-index.shtml


def limit_load_factors(
    design_mass_TOGW: float,
    category: str = "normal",
) -> Tuple[float, float]:
    """
    Computes the required limit load factors for FAR Part 23 certification.

    From FAR Part 23: "Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes"
    Section 23.337: "Limit maneuvering load factors"

    Args:

        design_mass_TOGW: The design takeoff gross weight of the aircraft [kg].

        category: The category of the aircraft. Valid values are:

            - "normal"
            - "utility"
            - "acrobatic"
            - "commuter"

    Returns:
        A tuple with (positive load factor, negative load factor). These are the maximum positive and negative limit load
        factors that the aircraft should withstand for Part 23 certification.

    """
    ### Compute positive load factor
    if category == "normal" or category == "commuter":
        positive_load_factor = np.softmin(
            2.1 + (24000 / (design_mass_TOGW / u.lbm + 10000)), 3.8, softness=0.01
        )
    elif category == "utility":
        positive_load_factor = 4.4

    elif category == "acrobatic":
        positive_load_factor = 6.0

    else:
        raise ValueError(
            "Bad value of `category`. Valid values are 'normal', 'utility', 'acrobatic', and 'commuter'."
        )

    ### Compute negative load factor
    if category == "normal" or category == "commuter" or category == "utility":
        negative_load_factor = -0.4 * positive_load_factor
    elif category == "acrobatic":
        negative_load_factor = -0.5 * positive_load_factor
    else:
        raise ValueError()

    return positive_load_factor, negative_load_factor