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fixed issue 27, AttributeError when calculating fuel flow for A21N #28

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fixed issue 27, AttributeError when calculating fuel flow for A21N #28

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3dfeaeb
fixed issue 27
Sep 16, 2024
5979b41
Corrected exception text
Sep 17, 2024
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6 changes: 4 additions & 2 deletions openap/fuel.py
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Original file line number Diff line number Diff line change
Expand Up @@ -46,6 +46,8 @@ def __init__(self, ac, eng=None, **kwargs):
if not hasattr(self, "WRAP"):
self.WRAP = importlib.import_module("openap.kinematic").WRAP

self.use_synonym = kwargs.get("use_synonym", False)

self.ac = ac.lower()
self.aircraft = prop.aircraft(ac, **kwargs)

Expand All @@ -65,7 +67,7 @@ def fuel_params(self):
"""Obtain the fuel model parameters.

Returns:
dict: drag polar model parameters.
dict: fuel model parameters.
"""
polar_files = glob.glob(dir_fuelmodel + "*.yml")
ac_polar_available = [pathlib.Path(s).stem for s in polar_files]
Expand All @@ -77,7 +79,7 @@ def fuel_params(self):
if self.use_synonym and syno.shape[0] > 0:
ac = syno.new.iloc[0]
else:
raise ValueError(f"Drag polar for {self.ac} not avaiable.")
raise ValueError(f"Fuel model for {self.ac} not avaiable.")

f = dir_fuelmodel + ac + ".yml"
with open(f, "r") as file:
Expand Down