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inpt18.m
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inpt18.m
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
% Copyright (C) 1999, 2007 Tomas Melin
%
% This file is part of Tornado
%
% Tornado is free software; you can redistribute it and/or
% modify it under the terms of the GNU General Public
% License as published by the Free Software Foundation;
% either version 2, or (at your option) any later version.
%
% Tornado is distributed in the hope that it will be useful,
% but WITHOUT ANY WARRANTY; without even the implied
% warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR
% PURPOSE. See the GNU General Public License for more
% details.
%
% You should have received a copy of the GNU General Public
% License along with Tornado; see the file GNU GENERAL
% PUBLIC LICENSE.TXT. If not, write to the Free Software
% Foundation, 59 Temple Place -Suite 330, Boston, MA
% 02111-1307, USA.
%
% usage: [GEO] = INPT (GEO)
%
% Invokes the geometry manipulation script of Tornado to allow
% the user to load, save, edit or input a new geometry structure.
% Geo is the structure containing all necessary geometrical
% definitions.
%
% Example:
%
% [geo]=inpt18(geo);
%
% Calls:
% questions Contain user interface queries in string format.
% terror Displays various Error messages.
% isinptok Checks format of imput.
% tedit Edit geo interface.
% f_version_geo_transform converts old geometry files to new standard.
%
% Author: Tomas Melin <[email protected]>
% Keywords: Tornado text based user interface
%
% Revision History:
% Bristol, 2007 06 27: Addition of new header. TM.
% Stockholm,2004 01 18: Changed all geometry variables to new format. TM.
% Added a "convert geometry file" function. TM.
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
function [geo]=inpt15(geo)
settings=config('startup'); %setting directories
loop1=1;
while loop1==1;
q=questions(2);
stat=0;
if isempty(q)
q=5; %will go to otherwise section
end
switch q
case 1 %enter new geometry
disp(' ')
ok1=0;
geo=[];
geo.flapped=0;
while ok1==0
data=input('Number of Wings: ','s');
if isinptok(data)==1;
geo.nwing=str2num(data);
ok1=1;
end
end
for s=1:geo.nwing %Stepping over the wings.
%home
disp('""""""""""""""""""""""""""""""""""""""""""""""""""""""')
disp('" ')
disp(strcat('" Data regarding wing number :', num2str(s),' '))
disp('" ')
disp('""""""""""""""""""""""""""""""""""""""""""""""""""""""')
disp(' ');
ok2=0;
while ok2==0
data=input('Number of semispanwise partitions for this wing: ','s');
if isinptok(data)==1;
geo.nelem(s)=str2num(data);
ok2=1;
end
end
t=0;
for s2=1:geo.nelem(s)
t=t+1;
disp(' ')
disp('""""""""""""""""""""""""""""""""""""""""""""""""""""""')
disp('" ')
disp(strcat('" Data regarding partition number: ',num2str(t),(' ')))
disp(' ')
if s==1
disp(' ')
disp('b - Back one question. ')
disp('q - Abort input sequence. ')
disp(' ')
end
stepper=-6;
while stepper<99
switch stepper
case -7
stepper=1;
case -6 %CG data added TM20070329
if s==1
if t==1;
data=input('Center of gravity x-coordinate: ','s');
if isinptok(data)==1;
geo.CG(1)=str2num(data);
end
end
end
case -5
if s==1
if t==1;
data=input('Center of gravity y-coordinate: ','s');
if isinptok(data)==1;
geo.CG(2)=str2num(data);
end
end
end
case -4
if s==1
if t==1;
data=input('Center of gravity z-coordinate: ','s');
if isinptok(data)==1;
geo.CG(3)=str2num(data);
end
end
end
case -3
if s==1
if t==1;
data=input('Reference point x-coordinate: ','s');
if isinptok(data)==1;
geo.ref_point(1)=str2num(data);
end
end
end
case -2
if s==1
if t==1;
data=input('Reference point y-coordinate: ','s');
if isinptok(data)==1;
geo.ref_point(2)=str2num(data);
end
end
end
case -1
if s==1
if t==1;
data=input('Reference point z-coordinate: ','s');
if isinptok(data)==1;
geo.ref_point(3)=str2num(data);
end
end
end
case 0
if t==1;
data=input('Is the wing mirrored in the xz-plane [1 0]: ','s');
if isinptok(data)==1;
geo.symetric(s)=str2num(data);
end
end
case 1
if s~=1
if t==1;
data=input('Apex x-coordinate: ','s');
if isinptok(data)==1;
geo.startx(s)=str2num(data);
end
end
else
geo.startx(s)=0;
end
case 2
if s~=1
if t==1;
data=input('Apex y-coordinate: ','s');
if isinptok(data)==1;
geo.starty(s)=str2num(data);
end
end
else
geo.starty(s)=0;
end
case 3
if s~=1
if t==1;
data=input('Apex z-coordinate: ','s');
if isinptok(data)==1;
geo.startz(s)=str2num(data);
end
end
else
geo.startz(s)=0;
end
case 4
if t==1;
data=input('Root chord: ','s');
if isinptok(data)==1;
geo.c(s)=str2num(data);
end
end
case 5
if t==1;
ok=0;
while ok==0;
try
cd(settings.afdir)
disp(' ')
disp('****************************** ')
disp(' AVAILABLE AIRFOILS: ')
ls
disp('****************************** ')
disp(' ')
disp('Enter profile filename from the list above (ex CLARKY.DAT) ')
disp('OR any NACA four digits series numer (ex: 2412)')
disp('0 (zero) for a flat plate. ')
disp(' ')
data=input('Base chord airfoil: ','s');
try
foo=str2num(data);
cd(settings.hdir)
catch
load(data) %Testload to see that the file exists
cd(settings.hdir)
end
geo.foil(s,t,1)={data};
data=0;
ok=1;
catch
cd(settings.hdir)
terror(4)
end
end
end
case 6
if t==1;
data=input('Number of panels chord wise: ','s');
if isinptok(data)==1;
geo.nx(s,1)=str2num(data);
end
end
case 7
if s==1 % First wing base chord is reference for twist
geo.TW(s,1,1)=0;
else
if t==1
data=input('Base chord twist [deg]: ','s');
if isinptok(data)==1;
geo.TW(s,1,1)=str2num(data)*pi/180;
end
end
end
case 8
%if t==1;
data=input('Partition dihedral [deg]: ','s');
if isinptok(data)==1;
geo.dihed(s,t)=str2num(data)*pi/180;
end
%end
case 9
data=input('Number of panels semi-span wise: ','s');
if isinptok(data)==1;
geo.ny(s,t)=str2num(data);
end
case 10
data=input('Span of partition: ','s');
if isinptok(data)==1;
geo.b(s,t)=str2num(data);
end
case 11
data=input('Taper ratio: ','s');
if isinptok(data)==1;
geo.T(s,t)=str2num(data);
end
case 12
ok=0;
while ok==0;
try
cd(settings.afdir)
disp(' ')
disp('****************************** ')
disp(' AVAILABLE AIRFOILS: ')
ls
disp('****************************** ')
disp(' ')
disp('Enter profile filename from the list above (ex CLARKY.DAT) ')
disp('OR any NACA four digits series numer (ex: 2412)')
disp('0 (zero) for a flat plate. ')
disp(' ')
data=input('Tip chord airfoil: ','s');
try
foo=str2num(data);
cd(settings.hdir)
catch
load(data) %Testload to see that the file exists
cd(settings.hdir)
end
geo.foil(s,t,2)={data};
data=0;
ok=1;
catch
cd(settings.hdir)
terror(4)
end
end
case 13
data=input('Quarter chord line sweep [deg]: ','s');
if isinptok(data)==1;
geo.SW(s,t)=str2num(data)*(pi/180);
end
case 14
data=input('Outboard twist [deg]: ','s');
if isinptok(data)==1;
geo.TW(s,t,2)=str2num(data)*(pi/180);
end
case 15
disp(' ')
disp(' *************** ')
disp(' Available mesh distribution types:')
disp(' [1] Linear')
disp(' [2] Spanwise half-cosine')
disp(' [3] Spanwise half-cosine, chordwise cosine')
disp(' [5] Spanwise cosine')
disp(' [6] Chordwise cosine')% (Added 22/08/2008 AT)
disp(' [7] 3:rd order centerpacking. (Not for wings)')
disp(' ')
data=input('Mesh type: ','s');
if isinptok(data)==1;
geo.meshtype(s,t)=str2num(data);
end
case 16
data=input('Is partition flapped [1 0]:','s');
if isinptok(data)==1;
geo.flapped(s,t)=str2num(data);
end
if geo.flapped==0;
stepper=100;
end
case 17
if geo.flapped(s,t)==1;
data=input('Flap chord in fraction of local chord (0..1): ','s');
if isinptok(data)==1;
geo.fc(s,t)=str2num(data);
end
end
case 18
if geo.flapped(s,t)==1;
data=input('Number of chord wise panels on flap: ','s');
if isinptok(data)==1;
geo.fnx(s,t)=str2num(data);
end
end
case 19
if and(geo.symetric(s),geo.flapped(s,t));
data=input('Do control surfaces deflect symmetrically [1 0]:','s');
if isinptok(data)==1;
geo.fsym(s,t)=str2num(data);
end
else
geo.fsym(s,t)=0;
end
end %caseblock
if isinptok(data)==1
stepper=stepper+1;
elseif isinptok(data)==-1
stepper=stepper-1;
elseif isinptok(data)==-2
stepper=99;
return
else
end
end% while partitionblock
if geo.flapped(s,t)==0
stepper=100;
geo.fc(s,t)=0;
geo.fnx(s,t)=0;
geo.fsym(s,t)=0;
end
geo.nx(s,t)=geo.nx(s,1);
%dihed(s,t)=dihed(s,1);
if t~=1
geo.TW(s,t,1)=geo.TW(s,t-1,2); %continious twist
geo.foil(s,t,1)=geo.foil(s,t-1,2); %continious camber
end
end%partitionblock
end%wingblock
geo.flap_vector=zeros(size(geo.flapped));
if isinptok(data)~=-2
loop1=0; %loop if aborted
end
case 2
geo=[];
lattice=[];
try
cd(settings.acdir)
ls
fname1=input('Load file: ','s');
load(fname1);
cd(settings.hdir)
%if isempty(geo.flap_vector) %remove this passus in version current +2
% geo.flap_vector=zeros(size(geo.flapped)); %fix for old geometry files
%end
if (tor_version)==126
disp(' ')
disp('*** WARNING! *** ')
disp(' ')
disp('Old geometry standard, NO geometry loaded. ')
disp('Please use geometry conversion function and reload.')
disp(' ')
return
end
loop1=0;
catch
cd(settings.hdir)
terror(4)
end
case(3)
[geo]=tedit(geo);
case(4)
cd(settings.acdir)
ls
tor_version=135;
fname2=input('Save file as: ','s');
if isempty(fname2)==1;
disp('+++ no name, not saved +++')
cd(settings.hdir)
else
try
save(fname2,'geo','tor_version') ;
disp('*** File Saved. ****');
cd(settings.hdir)
catch
cd(settings.hdir)
terror(5)
end
end
case(5)
%f_version_geo_transform;
geo=bodyinput(geo);
case 0
loop1=0;
otherwise
terror(9);
end
end