MIT-LAE / TASOPT.jl

Medium fidelity aircraft-propulsion system design and optimization.
https://mit-lae.github.io/TASOPT.jl/
MIT License
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Weight model documentation and write-up #30

Open argonaut22 opened 5 months ago

argonaut22 commented 5 months ago

Like for the other fields, we want to document the weight assumptions and provide a high-level summary for them (e.g., what scales with payload?, what's explicitly modelled? how are the different weight fractions normalized?). A placeholder page exists in the docs already