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