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List:       flightgear-cvs
Subject:    [Flightgear-cvslogs] CVS: source/src/Environment environment.cxx,
From:       Tim Moore <timoore () flightgear ! org>
Date:       2007-08-31 18:01:11
Message-ID: E1IRAnv-0005dw-00 () baron ! me ! umn ! edu
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Update of /var/cvs/FlightGear-0.9/source/src/Environment
In directory baron:/tmp/cvs-serv21685/src/Environment

Modified Files:
	environment.cxx 
Log Message:
Corrected atmosphere data, extended above 62000ft
Author: John Denker
Reviewed by: Ron Jensen and Gerard Robin


Index: environment.cxx
===================================================================
RCS file: /var/cvs/FlightGear-0.9/source/src/Environment/environment.cxx,v
retrieving revision 1.19
retrieving revision 1.20
diff -C 2 -r1.19 -r1.20
*** environment.cxx	29 Jul 2006 09:22:24 -0000	1.19
--- environment.cxx	31 Aug 2007 18:01:07 -0000	1.20
***************
*** 50,90 ****
  ////////////////////////////////////////////////////////////////////////
  
! // Copied from YASim Atmosphere.cxx, with m converted to ft, degK
! // converted to degC, Pa converted to inHG, and kg/m^3 converted to
! // slug/ft^3; they were then converted to deltas from the sea-level
! // defaults (approx. 15degC, 29.92inHG, and 0.00237slugs/ft^3).
! 
! // Original comment from YASim:
! 
! // Copied from McCormick, who got it from "The ARDC Model Atmosphere"
! // Note that there's an error in the text in the first entry,
! // McCormick lists 299.16/101325/1.22500, but those don't agree with
! // R=287.  I chose to correct the temperature to 288.20, since 79F is
! // pretty hot for a "standard" atmosphere.
  
! // Elevation (ft), temperature factor (degK), pressure factor (inHG)
  static double atmosphere_data[][3] = {
!  { 0.00, 1.00, 1.000 },
!  { 2952.76, 0.98, 0.898 },
!  { 5905.51, 0.96, 0.804 },
!  { 8858.27, 0.94, 0.719 },
!  { 11811.02, 0.92, 0.641 },
!  { 14763.78, 0.90, 0.570 },
!  { 17716.54, 0.88, 0.506 },
!  { 20669.29, 0.86, 0.447 },
!  { 23622.05, 0.84, 0.394 },
!  { 26574.80, 0.82, 0.347 },
!  { 29527.56, 0.80, 0.304 },
!  { 32480.31, 0.78, 0.266 },
!  { 35433.07, 0.76, 0.231 },
!  { 38385.83, 0.75, 0.201 },
!  { 41338.58, 0.75, 0.174 },
!  { 44291.34, 0.75, 0.151 },
!  { 47244.09, 0.75, 0.131 },
!  { 50196.85, 0.75, 0.114 },
!  { 53149.61, 0.75, 0.099 },
!  { 56102.36, 0.75, 0.086 },
!  { 59055.12, 0.75, 0.075 },
!  { 62007.87, 0.75, 0.065 },
   { -1, -1, -1 }
  };
--- 50,97 ----
  ////////////////////////////////////////////////////////////////////////
  
! // Calculated based on the ISA standard day, as found at e.g.
! // http://www.av8n.com/physics/altimetry.htm
  
! // Each line of data has 3 elements:
! //   Elevation (ft), 
! //   temperature factor (dimensionless ratio of absolute temp), 
! //   pressure factor (dimensionless ratio)
  static double atmosphere_data[][3] = {
!  {  -3000.00,   1.021,  1.1133 },
!  {      0.00,   1.000,  1.0000 },
!  {   2952.76,   0.980,  0.8978 },
!  {   5905.51,   0.959,  0.8042 },
!  {   8858.27,   0.939,  0.7187 },
!  {  11811.02,   0.919,  0.6407 },
!  {  14763.78,   0.898,  0.5697 },
!  {  17716.54,   0.878,  0.5052 },
!  {  20669.29,   0.858,  0.4468 },
!  {  23622.05,   0.838,  0.3940 },
!  {  26574.80,   0.817,  0.3463 },
!  {  29527.56,   0.797,  0.3034 },
!  {  32480.31,   0.777,  0.2649 },
!  {  35433.07,   0.756,  0.2305 },
!  {  38385.83,   0.752,  0.2000 },
!  {  41338.58,   0.752,  0.1736 },
!  {  44291.34,   0.752,  0.1506 },
!  {  47244.09,   0.752,  0.1307 },
!  {  50196.85,   0.752,  0.1134 },
!  {  53149.61,   0.752,  0.0984 },
!  {  56102.36,   0.752,  0.0854 },
!  {  59055.12,   0.752,  0.0741 },
!  {  62007.87,   0.752,  0.0643 },
!  {  65000.00,   0.752,  0.0557 },
!  {  68000.00,   0.754,  0.0482 },
!  {  71000.00,   0.758,  0.0418 },
!  {  74000.00,   0.761,  0.0362 },
!  {  77000.00,   0.764,  0.0314 },
!  {  80000.00,   0.767,  0.0273 },
!  {  83000.00,   0.770,  0.0237 },
!  {  86000.00,   0.773,  0.0206 },
!  {  89000.00,   0.777,  0.0179 },
!  {  92000.00,   0.780,  0.0156 },
!  {  95000.00,   0.783,  0.0135 },
!  {  98000.00,   0.786,  0.0118 },
!  { 101000.00,   0.789,  0.0103 },
   { -1, -1, -1 }
  };


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