ff33e631-4176-4470-85d1-554ad9ea6a18 11 4 5 decimal

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

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 - 64 s *

supersonic

subsonic

x 0 k 0.01 range :

u k 3 k 0.01 + (range :

sup u u Supersonic vectorize eval augment :

sub x x Subsonic vectorize augment k k Subsonic augment stack :

sub 00 0.01 0.1193 0.02 0.1684 0.03 0.2059 0.04 0.2374 0.05 0.2649 0.06 0.2897 0.07 0.3124 0.08 0.3334 0.09 0.353 0.1 0.3715 0.11 0.389 0.12 0.4056 0.13 0.4215 0.14 0.4367 0.15 0.4513 0.16 0.4654 0.17 0.479 0.18 0.4921 0.19 0.5048 0.2 0.5171 0.21 0.529 0.22 0.5406 232 mat

sup 0.8813 0.9947 0.8913 0.9993 0.9013 1.0038 0.9113 1.0082 0.9213 1.0127 0.9313 1.0171 0.9413 1.0215 0.9513 1.0258 0.9613 1.0301 0.9713 1.0344 0.9813 1.0387 0.9913 1.0429 1.0013 1.0471 1.0113 1.0513 1.0213 1.0554 1.0313 1.0595 1.0413 1.0636 1.0513 1.0677 1.0613 1.0717 1.0713 1.0757 1.0813 1.0797 1.0913 1.0837 1.1013 1.0877 232 mat

sub sup 0.8813 2 0.8813 1 - 2 2 mat 3 1 sys