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## Source directory # SUBDIRS = h_sources = thermo.h \ acentric_factor.h \ boiling_point.h \ critical_pressure.h \ critical_temperature.h \ density.h \ diffusion.h \ element.h \ element_name

// correct bug in CahuetChabard routine // sign of pressure correct // and change Bx, By in Bx' By' (back and forth) in version>1.18 // correction in CahouetChabard routine in version 1.26 asser

% Script file: ideal_gas.m % % Purpose: % This program plots the pressure versus volume of an % ideal gas. % % Record of revisions: % Date Programmer Description

# This demo solves the Stokes equations, using stabilized # first order elements for the velocity and pressure. The # sub domains for the different boundary conditions used # in this simulation are co

#HEXCOMMENT console - ver1.02 #include "console.h" #include "receiver.c" #define PLACE_MAX 8 #define MAX_PIXEL 7 #define MAX_NUMBER 10 #define NUMBER_WHEELS 5 #define NUMBER_PARAMETERS

function ind=linearppp(ind,params) %LINEARPPP Applies linear parametric parsimony pressure to a GPLAB individual. % LINEARPPP(INDIVIDUAL,PARAMS) returns the fitness of an individual % after

function res = source(z,holdon); % This program finds and plots the pressure distribution % on an airfoil by representing the surface as a finite % number of constant strength source panels. % (Neu

function res = doublet(z,alfa,holdon); % This program finds and plots the pressure distribution % on an airfoil by representing the surface as a finite % number of constant strength doublet panels.

# This demo solves the Stokes equations, using quadratic # elements for the velocity and first degree elements for # the pressure (Taylor-Hood elements). The sub domains # for the different boundary c

% Tempera- % Pressure Height Height ture Density % mb meters feet deg C kg / m**3 Comments atm=[ 1000.0 110.88 363.