initial release september 01 2001
new release november 27
2001 better user interface ; more tools
user friendly it will install over any existing issue
the install is the same as the old version
new release december 11
2001
-
added the save possibility with the "add to common log" button it will
create a text file containing the data of the current page in clear language
it will also save it on a big commonlog.txt file containing all the previously
saved files
-
added the possibility to print the screen (landscape format) there is
also the possibility to edit the text files and print them with any text
editor
-
added the "save as" possibility at the
main window it will create a text file containing the data of all the previously
saved files this is the same file as the commonlog.txt but with an other
name this way it will not be erased by the add to commonlog function . This
permit an easy comparison between project example :
cessna152longrange.txt and cessna152std_tank.txt
new release january 10
2002 (major release use all windows features)
new release january 13
2002 (minor release)
-
added the delete file menu it will only see , display and delete
the relevant *.dat and *.txt files it will not delete the individual
and common log txt files that can be useful and are re created on each "add
to common log"
Beta release February 28 2002
-
added the airfoil design file menu it permit to edit and modify
airfoil in order to pass it to other software such as X foil or panel for
windows . It display the airfoil to work on . It show small diagram
of the foil before opening them . There is the possibility to save some info
in one line of text in the airfoil dat file (first line) .
-
The airfoil can be scaled globally in the Y axis (thickness).
-
The airfoil can be modified by moving the vertex individually in
the Y axis (thickness)
-
The airfoil can be modified by moving the vertex by group in the
Y axis (thickness)
-
added a copy of airfoil data from uiuc under gnu licence plus other airfoils
to a total total of more than 1100 airfoils
-
corrected a bug in the jet section of the code of the "compute initial
design" menu
-
added colors to the flight envelope section
-
corrected some of the example files
Beta local computer march 18 2002
-
added faster drawing airfoil icon to the open foil section (the selected
airfoil is displayed)
-
added fast drawing polar icon to the open foil section (the selected
airfoil polar is displayed if available it should have the same name as the
airfoil but with a ".pol" ending :(xxxxx.pol) ) .
If no polar is available it will draw a straight line
-
added prototype pressure colors to the open foil section not finished
yet
Beta and base release debugged march 20 2002
-
erased a new call to a function that got here by error this function didn't
exist any more on the beta and current release and this was blocking
normal execution it was a call to a symantec function despite that
it is compiled with sun compiler ... I just zapped it !
-
on this day the current release and the beta release are the same
.
Beta local computer april 05 2002
-
added export to panel for windows function in order to run a 3D panel
wing check when finalized .
-
added export to ray tracer function in order to make the pov file needed
for rendering not finished yet
-
progressed in prototype pressure colors to the open foil section
still not finished yet
Beta release june 06 2002
-
made new functions to export to panel for windows .
-
now the export to ray tracer function can make the pov file for the wing
, horizontal tail , and vertical tail
-
added the singularity function it permit to have an idea of what are the
source the sink and the vortex. Those are the building block of the aerodynamic
and of the panel method . It permit to "play" with a source ; a
sink ; and a vortex and to grab the feel of how they behave
when associated together with a free stream creating a rankine oval
or a circle (cylinder) or circle with circulation (rotating cylinder).
This is not needed for airplane design but help to understand how
things works
-
finished the pressure colors coding but not released because it need a
pressure computation method (panel method)
-
begined to study a panel method 2d and 3d
-
corrected a bug : added the file : def.dat.pol in the foil directory
. it permit do draw the foil preview with default (straight) polar when none
are available