1057 225.66 K 100 a4 = 4 x 10-3 Km F90 80 +679 1165.66 K a3 = -4.5 X 10-3 K/m Altitude, km 282.66 K M a2 = 3 X 10-3 K/m 25- 71. Plot the density standard atmosphere in Matlab using SI units. You should be calcu- lating density using the appropriate e

The book is introduction to flight By Anderson

1057 225.66 K 100 a4 = 4 x 10-3 Km F90 80 +679 1165.66 K a3 = -4.5 X 10-3 K/m Altitude, km 282.66 K M a2 = 3 X 10-3 K/m 25- 701 = -6.5 X 10-3 K/m 11- 216.66 K 288.16 K 160 200 280 320 240 Temperature, K Figure 3.4 Temperature distribution in the standard atmosphere. 1. Plot the density standard atmosphere in Matlab using SI units. You should be calcu- lating density using the appropriate equations from Chapter 3 of Anderson, and other than equations, should only be using the gradient slopes from figure 3.4 in Anderson, sea level conditions, and the altitudes at which the standard atmosphere model changes from zone to zone (read: you should be calculating the temperature at each of those transition points, not taking them from the figure).



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