aerodynamic_analysis (schueltke): corrected wave drag calibration and neutral point estimation (!198) · Merge requests · UNICADO / Aircraft Design · GitLab

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Description

corrected wave drag calibration (the calibration is only applied, when the uncalibrated polar shows wave drag)
corrected function call of neutral point estimation with correct trimmed polar

Related Issue(s)

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Other Changes

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Screenshots/Logs

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Testing Instructions

download this branch and build aerodynamic_analysis
run module on already converged aircraft design
the output of drag polars for a delta stabilizer angle of 0 deg should be 0 in wave drag for the whole Ma=0.2 and Ma=0.5 polar. First wave drag occurrences from Ma=0.6 on (before also for Ma=0.2 and Ma=0.5 wave drag was calculated)
the neutral point should be equivalent to the design mass CG now for a trimmed polar (static_margin of 0)

Developer Checklist

Code has been tested locally and/or in pipeline.
Merge conflicts resolved with the target branch.

Additional Notes

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