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Pressure 的代码
co_refract.pro
;+
; NAME:
; CO_REFRACT()
;
; PURPOSE:
; Calculate correction to altitude due to atmospheric refraction.
;
; DESCRIPTION:
; CO_REFRACT can calculate both apparent altitude from obs
demoh2osat.m
function demoH2Osat
% demoH2OSat Fit saturation pressure versus temperature for water
%
% Synopsis: demoH2Osat
%
% Input: none
%
% Output: Print curve fit coefficients. Plot fit fcn vs. o
contents.m
% NMM Toolbox: data files
%
% airSat.dat Saturation pressure for air as a function of temperature
% Pressure (MPa) in column 1, Temperature (K) in column 2
% airvisc.dat
emission.dat
Nitrogen oxide emission (parts per million) from an internal combustion engine as function
of humidity (grains per pound of dry air) and atmospheric pressure (inches of Hg).
Data from Example 13.6,
demoh2osat.m
function demoH2Osat
% demoH2OSat Fit saturation pressure versus temperature for water
%
% Synopsis: demoH2Osat
%
% Input: none
%
% Output: Print curve fit coefficients. Plot fit fcn vs. o
contents.m
% NMM Toolbox: data files
%
% airSat.dat Saturation pressure for air as a function of temperature
% Pressure (MPa) in column 1, Temperature (K) in column 2
% airvisc.dat
emission.dat
Nitrogen oxide emission (parts per million) from an internal combustion engine as function
of humidity (grains per pound of dry air) and atmospheric pressure (inches of Hg).
Data from Example 13.6,
atmosphere.txt
% function [t, p, rho, a] = atmosphere(height, unit)
% Richard Rieber
% rrieber@gmail.com
% Updated 3/17/2006
%
% Function to determine temperature, pressure, density, and speed of sound
% as a
stokesuzawa.edp
// signe of pressure is correct
assert(version>1.18);
real s0=clock();
mesh Th=square(10,10);
fespace Xh(Th,P2),Mh(Th,P1);
Xh u1,u2,v1,v2;
Mh p,q,ppp;
varf bx(u1,q) = int2d(Th)( (dx(u1)*q));
va
ex-vf.edp
// signe of pressure if correct
assert(version>1.18);
mesh Th=square(10,10);
fespace Xh(Th,P2),Mh(Th,P1);
Xh u1,u2,v1,v2;
Mh p,q,ppp;
varf bx(u1,q) = int2d(Th)( (dx(u1)*q));
varf by(u1,q) = int