Initial test "FlyingWing" after MachUp installation

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Peter Kämpf

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Jul 28, 2024, 3:30:23 AM7/28/24

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Hi,

I just installed MachUp from https://github.com/usuaero/MachUp/tree/dev_lowra and ran the initial test. It does not report any error, but also does not produce a result file or any results beyond a geometry analysis.

peter@MBP2023 FlyingWing % ./Machup input.json

-----------------------------------------------

| |

| BBBBB |

| BB BB |

| BB BBBBBB |

| |

| MachUp 1.0 |

| |

| (c) USU Aero Lab, LLC, 2016 |

| |

| This software comes with |

| ABSOLUTELY NO WARRANTY EXPRESSED OR IMPLIED |

| |

| Submit bug reports to: |

| doug.h...@usu.edu |

-----------------------------------------------

Reading Input File...

condition.omega.roll set to 0.0000000000000000

condition.omega.pitch set to 0.0000000000000000

condition.omega.yaw set to 0.0000000000000000

solver.maxiter set to 100

Airfoil database located at: ../AirfoilDatabase

Number of controls : 2

: aileron 0.0000000000000000 (deg)

: elevator 0.0000000000000000 (deg)

Reading airfoil properties from file: ../AirfoilDatabase/NACA_2410.json

Loaded airfoil: NACA_2410

Reading airfoil properties from file: ../AirfoilDatabase/NACA_4410.json

Loaded airfoil: NACA_4410

wings.wing_1.root_clustering set to 1

wings.wing_1.tip_clustering set to 1

Successfully read input file.

Wing properties for wing named: wing_1

Span : 4.0000000000000000

Area : 4.0000000000000000

Using Sweep Definition: 1

Wing properties for wing named: wing_1

Span : 4.0000000000000000

Area : 4.0000000000000000

Using Sweep Definition: 1

CPU time total (sec): 2.6270000000000009E-003

peter@MBP2023 FlyingWing %

BTW, I get the same result with the master branch. So what is missing here? Why does the test get stuck in the initial step?