788c6517-dfb8-4d1b-9eb2-0e88cae52932 7 4 5 decimal

&[DATE] &[TIME] - &[FILENAME]

4 appVersion 0.98.6179.21440 ≡

Speed of sound for water @ 20°C, 1 atm A T 20 °C * P 1 atm * Water CoolProp_Props 1482.3462 m s / *

v 0.001 30 0.1 range :

speed A T 200 °C * P v atm * Water CoolProp_Props vectorize :

data v speed m s / / augment :

data

v 103011 range :

speed A T 200 °C * P v atm * Water CoolProp_Props vectorize :

data v speed m s / / augment :

data

data 10 517.1 11 514.9 12 512.7 13 510.3 14 507.7 15 504.9 16 1332.3 17 1332.7 18133319 1333.4 20 1333.8 21 1334.2 22 1334.5 23 1334.9 24 1335.3 25 1335.6 26133627 1336.4 28 1336.7 29 1337.1 30 1337.5 212 mat

v 0.1 20 0.2 range :

speed A T 200 °C * P v atm * Air CoolProp_Props vectorize :

data v speed m s / / augment :

data

data 0.1 434.4 0.2 434.4 0.3 434.5 0.4 434.5 0.5 434.5 0.6 434.5 0.7 434.5 0.8 434.6 0.9 434.6 1 434.6 1.1 434.6 1.2 434.7 1.3 434.7 1.4 434.7 1.5 434.7 1.6 434.7 1.7 434.8 1.8 434.8 1.9 434.8 2 434.8 2.1 434.9 2.2 434.9 2.3 434.9 232 mat

v 1300 range :

Air A T 10 °C * P v atm * Air CoolProp_Props vectorize :

data v Air m s / / augment :

data

data 1 337.4 2 337.5 3 337.6 4 337.7 5 337.8 6 337.9 73388 338.1 9 338.2 10 338.3 11 338.4 12 338.5 122 mat

γ 1.4 : (Air isentropic ≡ k 0.88128485 : (Pitot constant ≡ p static pressure ≡ qc dynamic pressure ≡ x Pitot dynamic ratio qc/P ≡ x qc p / ≡ (supersonic Pitot ratio ≡ 61 line

Observe the canvas solutions:

as 'x' in Supersonic(x) runs on the plot canvas,

the 'roots' solves and plots each canvas pixel result ...

each result on the basis of 96 ppi [pixel per inch].

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Plot limit x c 10 x ≤ (x 5 ≤ (& cases :

t0 1 time :

x Subsonic 2 γ 1 - / (x 1 + (γ 1 - γ /^1 - (* sqrt 0 x ≤ (x k ≤ (& Supersonic cases : x Supersonic U x 1 + (117 U 2^* / - (2.5^* sqrt / k - 0 ≡ U 1 roots k x ≤ Subsonic cases : 21 line

x Subsonic x Supersonic x c * k 1 + 20 black 1 5 mat 3 1 sys

1 time t0 - 70 s *

supersonic

subsonic