[Libreoffice-bugs] [Bug 141008] New: copy of parts of website in LO writer -> frozen writer, impress ok

[bugzilla-daemon at bugs.documentfoundation.org]

https://bugs.documentfoundation.org/show_bug.cgi?id=141008

            Bug ID: 141008
           Summary: copy of parts of website in LO writer -> frozen
                    writer, impress ok
           Product: LibreOffice
           Version: 7.1.1.2 release
          Hardware: All
                OS: All
            Status: UNCONFIRMED
          Severity: normal
          Priority: medium
         Component: Writer
          Assignee: libreoffice-bugs at lists.freedesktop.org
          Reporter: paulystefan at web.de

copy of parts of the website in LO writer 

WYSIWYG is ideal for this. No problem for MSO 2016 for Text and links.

Version: 7.1.1.2 (x64) / LibreOffice Community
Build ID: fe0b08f4af1bacafe4c7ecc87ce55bb426164676
CPU threads: 8; OS: Windows 10.0 Build 19042; UI render: Skia/Raster; VCL: win
Locale: de-DE (de_DE); UI: de-DE
Calc: CL

>From https://sourceforge.net/projects/construct2d/

After the copy action of this text from the website with Strg C and Strg V
below, LO Writer is frozen, Impress can do it.

Construct2D is a grid generator designed to create 2D grids for CFD
computations on airfoils. The grids are generated in Plot3D format. The only
required input file is the set of coordinates defining the airfoil geometry,
using the same format as XFoil, the popular vortex-panel code for airfoil
analysis. Construct2D can create grids with O topology (recommended for
airfoils with a blunt trailing edge) or C topology (recommended for airfoils
with a sharp trailing edge). Now available in version 2.0: hyperbolic grid
generation to create higher quality grids in a fraction of the time compared to
elliptic grid generation. Elliptic grid generation is still available also.
Smooth airfoil surface spacing is handled automatically with user-controlled
clustering parameters. Also included is a visualizer written in Python with
matplotlib.
Features

    2D structured grid generation designed for airfoils
    3D grid (extruded 2D planes) output capability
    Hyperbolic grid generation is now available (v2.0) for fast, high-quality
grids
    Elliptic (poisson equation) grid generation is also available
    C-grid or O-grid capability
    Simple geometry input file format
    Handles blunt or sharp trailing edges
    Paneling subroutines adapted from XFoil for smooth distribution of points
on the airfoil surface
    Menu-driven or input-file-driven
    "PostPycess" script: grid and solution visualization with python &
matplotlib
    New in v2.0.4: Writes out a boundary condition file in NASA neutral map
(.nmf) format.

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