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I'm currently doing some validations on aircraft performance with the openAP model of BS, since I did not find much information, I'm trying to figure out if there is any way to obtain the weight of the plane. Fuel weight or gross weight. ex bs.traf.perf.fuelflow. Or establish an initial weight when creating a scenario.
I already checked on the perfoap.py and did not find anything about weight. Also, it will be helpful to know if there is a predefined weight of the aircraft since I did not find it on the A333 document in wrap folder.
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Hello,
I'm currently doing some validations on aircraft performance with the openAP model of BS, since I did not find much information, I'm trying to figure out if there is any way to obtain the weight of the plane. Fuel weight or gross weight. ex bs.traf.perf.fuelflow. Or establish an initial weight when creating a scenario.
I already checked on the perfoap.py and did not find anything about weight. Also, it will be helpful to know if there is a predefined weight of the aircraft since I did not find it on the A333 document in wrap folder.
The aircraft I am using is the A333
Thank you in advance.
Uri
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