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Next: Open Valve maximum values Up: Normal Shock Standard tables Previous: Normal Shock Standard Table   Contents

Normal shock Standard Table for k=1.67

Normal Shock Input: Mx k = 1.67
Mx My Ty/Tx ρy/ρx Py/Px P0y/P0x
1 1 1 1 1 1
1.01 0.990148 1.01001 1.01498 1.02514 0.999999
1.02 0.980583 1.01998 1.02996 1.05054 0.99999
1.03 0.971293 1.02991 1.04493 1.07618 0.999968
1.04 0.962267 1.0398 1.0599 1.10208 0.999927
1.05 0.953493 1.04965 1.07485 1.12822 0.99986
1.06 0.944961 1.05948 1.0898 1.15462 0.999763
1.07 0.936661 1.06927 1.10473 1.18126 0.999632
1.08 0.928585 1.07905 1.11965 1.20816 0.999462
1.09 0.920722 1.0888 1.13455 1.2353 0.999249
1.1 0.913066 1.09854 1.14943 1.2627 0.998991
1.2 0.846289 1.19555 1.29682 1.55041 0.993354
1.25 0.81843 1.24424 1.36923 1.70365 0.988163
1.3 0.79351 1.29334 1.44057 1.86315 0.981296
1.35 0.771108 1.34302 1.5107 2.0289 0.972773
1.4 0.750876 1.39341 1.5795 2.2009 0.962663
1.45 0.73253 1.44465 1.64688 2.37916 0.951068
1.5 0.715834 1.49681 1.71276 2.56367 0.938111
1.55 0.700587 1.54998 1.77708 2.75444 0.923926
1.6 0.686621 1.60423 1.83979 2.95146 0.908655
1.65 0.673792 1.65963 1.90087 3.15474 0.89244
1.7 0.661977 1.71621 1.96029 3.36427 0.87542
1.75 0.65107 1.77402 2.01805 3.58006 0.857732
1.8 0.640977 1.8331 2.07413 3.8021 0.839502
1.85 0.631619 1.89348 2.12856 4.03039 0.82085
1.9 0.622924 1.95519 2.18134 4.26494 0.801887
1.95 0.614831 2.01825 2.2325 4.50575 0.782714
2 0.607284 2.08269 2.28205 4.75281 0.763424
2.1 0.593643 2.21576 2.37647 5.26569 0.724814
2.2 0.581671 2.35453 2.46487 5.8036 0.686615
2.3 0.571106 2.49909 2.54754 6.36652 0.649256
2.4 0.561736 2.64952 2.6248 6.95446 0.613058
2.5 0.553386 2.8059 2.69697 7.56742 0.578246
2.6 0.545915 2.96826 2.76438 8.20539 0.544969
2.7 0.539202 3.13665 2.82735 8.86839 0.513317
2.8 0.533151 3.3111 2.88617 9.5564 0.483329
2.9 0.527676 3.49166 2.94114 10.2694 0.45501
3 0.522707 3.67833 2.99253 11.0075 0.428336
3.5 0.503621 4.70406 3.20426 15.073 0.317715
4 0.490964 5.8848 3.35849 19.764 0.238392
4.5 0.482154 7.22136 3.4731 25.0805 0.181634
5 0.475781 8.71418 3.56 31.0225 0.140646
5.5 0.471026 10.3635 3.62715 37.5899 0.110633
6 0.467386 12.1694 3.67994 44.7828 0.0883149
6.5 0.464539 14.1321 3.7221 52.6011 0.0714596
7 0.462271 16.2516 3.75624 61.0449 0.0585392
7.5 0.460435 18.5279 3.78425 70.1142 0.0484956
8 0.458928 20.9611 3.80749 79.809 0.0405863
8.5 0.457677 23.5511 3.82696 90.1292 0.0342827
9 0.456627 26.2981 3.84343 101.075 0.0292032
9.5 0.455736 29.2019 3.85749 112.646 0.0250682
10 0.454975 32.2627 3.86957 124.843 0.0216705
20 0.449663 126.436 3.95556 500.124 0.00288462
25 0.449023 197.065 3.96613 781.584 0.00149134
30 0.448675 283.389 3.9719 1125.59 0.000868412
35 0.448465 385.408 3.97539 1532.15 0.000549283
40 0.448328 503.123 3.97765 2001.25 0.000369214
45 0.448235 636.532 3.97921 2532.9 0.00026001
50 0.448168 785.637 3.98032 3127.09 0.000189973
55 0.448118 950.438 3.98115 3783.83 0.000143003
60 0.448081 1130.93 3.98177 4503.12 0.000110334
65 0.448051 1327.12 3.98226 5284.96 8.69096e-5
70 0.448028 1539.01 3.98265 6129.34 6.96779e-5


Created by:Genick Bar-Meir, Ph.D.
On: 2007-12-04


These tables were generated using Potto-GDC (gas dynamics calculator) and also available in pdf version.



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