Dataset in support of the thesis 'Credibility-based optimisation of (Hybrid-) Electric Aircraft '

Data is available 'on request' please complete the form at https://library.soton.ac.uk/datarequest

This dataset contains results presented in the thesis 'Credibility-based optimisation of (Hybrid-) Electric Aircraft '. The dataset contains 3 folders:

1. Credibility: Python files used to create the credibility curves for laminar flow and structural weight reductions.

2. Networks: SUAVE simulation results for all variants used in the sensitivity studies for the boosted-turbofan aircraft and the fully-electric aircraft.

3. TMS: SUAVE simulation results for all variants used in the sensitivity studies for both TMS architectures (with and without skin heat exchanger).