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Next: Isothermal Nozzle for k=1.3 Up: Isothermal Nozzle Previous: Isothermal Nozzle   Contents

Isothermal Nozzle for k=1.2

Isothermal Nozzle Flow Input: M k = 1.2
M T0/T0* P0/P0* A/A* P/P* PAR F/F*
1e-6 0.909091 1.02854 548812 1.82212 1e+6 454545
0.0500005 0.909318 1.02854 10.9926 1.81939 19.9998 9.11809
0.1 0.91 1.02854 5.52114 1.81122 10 4.6
0.2 0.912727 1.02849 2.81071 1.77891 5 2.38182
0.25 0.914773 1.02842 2.27913 1.75505 4 1.95455
0.3 0.917273 1.02829 1.93087 1.72633 3.33333 1.67879
0.35 0.920227 1.02808 1.68762 1.693 2.85714 1.48961
0.4 0.923636 1.02776 1.51027 1.65533 2.5 1.35455
0.45 0.9275 1.02729 1.37714 1.61365 2.22222 1.25556
0.5 0.931818 1.02664 1.27526 1.56831 2 1.18182
0.55 0.936591 1.02577 1.19642 1.51968 1.81818 1.12645
0.6 0.941818 1.02464 1.13522 1.46815 1.66667 1.08485
0.65 0.9475 1.02319 1.08794 1.41411 1.53846 1.05385
0.7 0.953636 1.02139 1.05198 1.35798 1.42857 1.03117
0.75 0.960227 1.01917 1.0255 1.30018 1.33333 1.01515
0.8 0.967273 1.01649 1.00717 1.2411 1.25 1.00455
0.85 0.974773 1.01328 0.996027 1.18116 1.17647 0.998396
0.9 0.982727 1.0095 0.991398 1.12075 1.11111 0.99596
0.95 0.991136 1.00509 0.992819 1.06024 1.05263 0.996651
1 1 1 1 1 1 1
1.05 1.00932 0.994167 1.01279 0.940353 0.952381 1.00563
1.1 1.01909 0.987544 1.03117 0.881615 0.909091 1.01322
1.15 1.02932 0.980081 1.05521 0.82407 0.869565 1.02253
1.2 1.04 0.971732 1.08511 0.767974 0.833333 1.03333
1.25 1.05114 0.962454 1.12115 0.713552 0.8 1.04545
1.3 1.06273 0.952211 1.16374 0.661001 0.769231 1.05874
1.35 1.07477 0.940969 1.21336 0.610486 0.740741 1.07306
1.4 1.08727 0.928704 1.27065 0.562142 0.714286 1.08831
1.45 1.10023 0.915395 1.33634 0.516077 0.689655 1.10439
1.5 1.11364 0.901031 1.41133 0.472367 0.666667 1.12121
1.55 1.1275 0.885606 1.49667 0.431063 0.645161 1.13871
1.6 1.14182 0.869125 1.5936 0.392193 0.625 1.15682
1.65 1.15659 0.851599 1.70357 0.35576 0.606061 1.17548
1.7 1.17182 0.833051 1.82827 0.321744 0.588235 1.19465
1.75 1.1875 0.813509 1.96971 0.290109 0.571429 1.21429
1.8 1.20364 0.793012 2.13019 0.2608 0.555556 1.23434
1.85 1.22023 0.771609 2.31247 0.233751 0.540541 1.25479
1.9 1.23727 0.749355 2.51972 0.208879 0.526316 1.2756
1.95 1.25477 0.726314 2.7557 0.186095 0.512821 1.29674
2 1.27273 0.702558 3.02482 0.165299 0.5 1.31818
2.25 1.36932 0.576015 5.0864 0.087379 0.444444 1.42929
2.5 1.47727 0.445386 9.33443 0.0428521 0.4 1.54545
2.75 1.59659 0.322944 18.651 0.0194969 0.363636 1.66529
3 1.72727 0.218551 40.5035 0.00822975 0.333333 1.78788
3.25 1.86932 0.13751 95.4731 0.00322282 0.307692 1.91259
3.5 2.02273 0.080193 244.017 0.00117088 0.285714 2.03896
3.75 2.1875 0.043242 675.697 0.000394654 0.266667 2.16667
4 2.36364 0.0215196 2025.77 0.00012341 0.25 2.29545
4.25 2.55114 0.00986989 6572.05 3.58022e-5 0.235294 2.42513
4.5 2.75 0.00416769 23061.6 9.63604e-6 0.222222 2.55556
4.75 2.96023 0.00161907 87496.6 2.40611e-6 0.210526 2.6866
5 3.18182 0.000578378 358815 5.5739e-7 0 2.81818
5.25 3.41477 0.000189934 1.59004e+6 1.19793e-7 0 2.95022
5.5 3.65909 5.73286e-5 7.61212e+6 2.38854e-8 0 3.08264
5.75 3.91477 1.59037e-5 3.93616e+7 4.41835e-9 0 3.21542
6 4.18182 4.05515e-6 2.19803e+8 7.58256e-10 0 3.34848
6.25 4.46023 9.50477e-7 1.32532e+9 1.20726e-10 0 3.48182
6.5 4.75 2.0482e-7 8.6273e+9 1.78325e-11 0 3.61538
6.75 5.05114 4.05869e-8 6.0624e+10 2.44372e-12 0 3.74916
7 5.36364 7.39733e-9 4.59815e+11 3.10684e-13 0 3.88312
7.25 5.6875 1.24035e-9 3.76398e+12 3.6645e-14 0 4.01724
7.5 6.02273 1.9138e-10 3.32507e+13 4.00994e-15 0 4.15152
7.75 6.36932 2.71798e-11 3.16963e+14 4.07089e-16 0 4.28592
8 6.72727 3.55388e-12 3.26018e+15 3.83415e-17 0 4.42045
8.25 7.09659 4.27932e-13 3.61801e+16 3.35024e-18 0 4.5551
8.5 7.47727 4.74646e-14 4.33182e+17 2.71588e-19 0 4.68984
8.75 7.86932 4.85061e-15 5.59523e+18 2.04256e-20 0 4.82468
9 8.27273 4.56833e-16 7.79637e+19 1.42516e-21 0 4.9596
9.25 8.6875 3.966e-17 1.17186e+21 9.22537e-23 0 5.09459
9.5 9.11364 3.17454e-18 1.89997e+22 5.54026e-24 0 5.22967
9.75 9.55114 2.34334e-19 3.32269e+23 3.08678e-25 0 5.3648
10 10 1.59554e-20 6.26747e+24 1.59554e-26 0 5.5
20 37.2727 2.87242e-95 4.66733e+102 1.07128e-104 0 10.9318
30 82.7273 1.76786e-223 6.04397e+232 5.51514e-235 0 16.3788
40 146.364 0 inf 0 0 21.8295
50 228.182 0 inf 0 0 27.2818
Table 2.2: Isothermal Table
$ \rule[-.1in]{0.pt}{0.3 in}\mathbf{M} $ $ \mathbf{T_0 \over {T_0}^{\star}} $ $ \mathbf{P_0 \over {P_0}^{\star}} $ $ \mathbf{A \over A^{\star}} $ $ \mathbf{P \over P^{\star}} $ $ \mathbf{A\times P \over A^{*} \times P_0} $ $ \mathbf{F \over F^{*}} $
0.00 0.52828 1.064 5.0E+5 2.014 1.0E+6 4.2E+5
0.05 0.52921 1.064 9.949 2.010 20.00 8.362
0.1 0.53199 1.064 5.001 2.000 10.00 4.225
0.2 0.54322 1.064 2.553 1.958 5.000 2.200
0.3 0.56232 1.063 1.763 1.891 3.333 1.564
0.4 0.58985 1.062 1.389 1.800 2.500 1.275
0.5 0.62665 1.059 1.183 1.690 2.000 1.125
0.6 0.67383 1.055 1.065 1.565 1.667 1.044
0.7 0.73278 1.047 0.99967 1.429 1.429 1.004
0.8 0.80528 1.036 0.97156 1.287 1.250 0.98750
0.9 0.89348 1.021 0.97274 1.142 1.111 0.98796
1.00 1.000 1.000 1.000 1.000 1.000 1.000
1.10 1.128 0.97376 1.053 0.86329 0.90909 1.020
1.20 1.281 0.94147 1.134 0.73492 0.83333 1.047
1.30 1.464 0.90302 1.247 0.61693 0.76923 1.079
1.40 1.681 0.85853 1.399 0.51069 0.71429 1.114
1.50 1.939 0.80844 1.599 0.41686 0.66667 1.153
1.60 2.245 0.75344 1.863 0.33554 0.62500 1.194
1.70 2.608 0.69449 2.209 0.26634 0.58824 1.237
1.80 3.035 0.63276 2.665 0.20846 0.55556 1.281
1.90 3.540 0.56954 3.271 0.16090 0.52632 1.328
2.00 4.134 0.50618 4.083 0.12246 0.50000 1.375
2.50 9.026 0.22881 15.78 0.025349 0.40000 1.625
3.000 19.41 0.071758 90.14 0.00370 0.33333 1.889
3.500 40.29 0.015317 7.5E+2 0.000380 0.28571 2.161
4.000 80.21 0.00221 9.1E+3 2.75E-5 0.25000 2.438
4.500 1.5E+2 0.000215 1.6E+5 1.41E-6 0.22222 2.718
5.000 2.8E+2 1.41E-5 4.0E+6 0.0 0.20000 3.000
5.500 4.9E+2 0.0 1.4E+8 0.0 0.18182 3.284
6.000 8.3E+2 0.0 7.3E+9 0.0 0.16667 3.569
6.500 1.4E+3 0.0 5.3E+11 0.0 0.15385 3.856
7.000 2.2E+3 0.0 5.6E+13 0.0 0.14286 4.143
7.500 3.4E+3 0.0 8.3E+15 0.0 0.13333 4.431
8.000 5.2E+3 0.0 1.8E+18 0.0 0.12500 4.719
8.500 7.7E+3 0.0 5.4E+20 0.0 0.11765 5.007
9.000 1.1E+4 0.0 2.3E+23 0.0 0.11111 5.296
9.500 1.6E+4 0.0 1.4E+26 0.0 0.10526 5.586
10.00 2.2E+4 0.0 1.2E+29 0.0 0.100000 5.875


next up previous contents
Next: Isothermal Nozzle for k=1.3 Up: Isothermal Nozzle Previous: Isothermal Nozzle   Contents
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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