Segmentation fault (core dumped)

[Tupuuducuu]

Hi,

first thank you for developing this code, I'm very curious to see what I can do with it. I have just downloaded, and I wanted to test the tutorials.

It loads all the input but it finish by an error message. Can you help me please ?

queue info: file problems is found
queue info: file defaults is found
queue info: file switchers is found

queue info: Number of problems to be solved: 1

queue info: -------- Loading problem #0 (circle200) --------
queue->problem parameters info: parameter <pspfile = passport> set as default
queue->problem parameters info: parameter <copyPath = > set as default
queue->#0 (circle200) passport info: file ./circle200/passport is found
queue->#0 (circle200) passport info: file defaults is found
queue->#0 (circle200) passport info: file switchers is found
queue->#0 (circle200) passport info: file mechanics is found
queue->#0 (circle200) passport->parser info: parameter <vRef = 0> set as default
queue->#0 (circle200) passport->parser info: parameter <timeStart = 0> set as default
queue->#0 (circle200) passport->parser info: parameter <rotateVpPoints = 0> set as default
queue->#0 (circle200) passport->parser info: parameter <saveVisStress = 0> set as default
queue->#0 (circle200) passport->parser info: parameter <fileWake = > set as default
queue->#0 (circle200) passport->parser info: parameter <fileSource = > set as default
queue->#0 (circle200) passport->parser info: parameter <geographicalAngles = 0> set as default
queue->#0 (circle200) passport->parser info: parameter <rotateForces = 0> set as default
queue->#0 (circle200) passport->airfoil parser info: parameter <nPanels = 0> set as default
queue->#0 (circle200) passport->airfoil parser info: parameter <addedMass = { 0, 0 }> set as default
queue->#0 (circle200) passport->airfoil parser info: parameter <inverse = 0> set as default
queue->#0 (circle200) passport info: --- Passport info ---
rho = 1
vInf = { 1, 0 }
vRef = 1
velAccel = RampLin( 0 )
nu = 0.005
timeStart = 0
timeStop = 500
dt = 0.01
nameLength = 5
saveVtx = binary( 100 )
saveVP = binary( 100 )
saveVisStress = 0
eps = 0.0075
eps2 = 5.625e-05
epscol = 0.005
distFar = 20
delta = 5e-06
vortexPerPanel = 1
maxGamma = 0
linearSystemSolver = linearSystemGauss
velocityComputation = velocityBiotSavart
boundaryCondition = boundaryConstantLayerAverage
airfoilsDir = ../settings/airfoils/
wakesDir = ../settings/wakes/
geographicalAngles = 0
rotateForces = 0
calcCoefficients = 1
rotateVpPoints = 0
number of airfoils = 1
airfoil[0]_file = circle200
airfoil[0]_requiredNPanels = 0
airfoil[0]_basePoint = { 0, 0 }
airfoil[0]_scale = { 1, 1 }
airfoil[0]_angle = 0
airfoil[0]_chord = 1
airfoil[0]_inverse = false
airfoil[0]_mechanicalSystem = mech0
airfoil[0]_addedMass = { 0, 0 }
fileWake =
fileSource =
queue info: -------- Problem #0 (circle200) is loaded --------

queue info: ProcStates:
proc[0] <=> problem[0]

#0 (circle200) info: file ./circle200/pointsVP is found
#0 (circle200) info: file ../settings/airfoils/circle200 is found

#0 (circle200) info: Start solving problem circle200

/--------------------------------- VM2D ---------------------------------*
| ## ## ## ## #### ##### | | Version 1.12 |
| ## ## ### ### ## ## ## ## | VM2D: Vortex Method | 2024/01/14 |
| ## ## ## # ## ## ## ## | for 2D Flow Simulation ----------------
| #### ## ## ## ## ## | Open Source Code |
| ## ## ## ###### ##### | https://www.github.com/vortexmethods/VM2D |
| |
| Copyright (C) 2017-2024 I. Marchevsky, K. Sokol, E. Ryatina, A. Kolganova |
-----------------------------------------------------------------------------
#0 (circle200) info: Preparing VP points
Segmentation fault (core dumped)