Source code for aerosandbox.library.weights.raymer_fudge_factors
# From Raymer, Aircraft Design: A Conceptual Approach, 5th Ed.
# Table 15.4
advanced_composites = {
# Format:
# "component" : (low, high)
"wing" : (0.85, 0.90),
"tails" : (0.83, 0.88),
"fuselage/nacelle" : (0.90, 0.95),
"landing_gear" : (0.95, 1),
"air_induction_system": (0.85, 0.90),
}
[docs]advanced_composites = { # Here, we convert this to a dictionary of average values.
k: (v[0] + v[1]) / 2
for k, v in advanced_composites.items()
}