MachUp

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i dont know

hunterbs123

section_alpha_L0 is incorrect in output file "input_distributions.txt" when using non-linear airfoil properties.

marcovanderbijl

unable to produce correct stl file when using sweep_file table input

2

I was trying to recreate the wing as showcased in the research paper "Wing optimisation using Dual Number Automatic Differentiation in MachUp". That used a sweep table input file. MachUp...

marcovanderbijl

#HacktoberFest2018

hunterbs123

Running the tests with python2.7 or python3, several of the test cases fail with the following warning in `def _calc_segment_points()`: pos = np.rot90(np.array([z_pos, y_pos, x_pos]), axes=(1, 0)) E TypeError: rot90()...

dalon-work