www.pudn.com > WebsiteCode.zip > wingnested4.m, change:2008-07-24,size:1888b

% Another example of using nested4.m, this time using the
% lifting surface weight example
%
% Baseline values
% S_w    -Wing area (ft^2)                              174
% W_fw   -Weight of fuel in the wing (lb)               252
% A      -aspect ratio                                 7.52
% Lambda -quarter-chord sweep (deg)                       0
% q      -dynamic pressure at cruise (lb/ft^2)           34
% lambda -taper ratio                                 0.672
% tc     -aerofoil thickness to chord ratio            0.12
% W_dg   -flight design gross weight (lb)             ~2000
% W_p    -paint weight (lb/ft^2)                     ~0.064
%
%
% This program is free software: you can redistribute it and/or modify  it
% the Free Software Foundation, either version 3 of the License, or any
% later version.
%
% This program 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 Lesser
% General Public License for more details.
%
% You should have received a copy of the GNU General Public License and GNU
% Lesser General Public License along with this program. If not, see

100, 151.17117, 414.20208, 0)