Gas Dynamics Tables Free Textbook

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Normal Shock Standard Table for k=1.2

Normal Shock		Input: Mx		k = 1.2
Mx	My	Ty/Tx	ρy/ρx	Py/Px	P0y/P0x
1	1	1	1	1	1
1.01	0.990117	1.00362	1.01824	1.02193	0.999999
1.02	0.980462	1.00722	1.03659	1.04407	0.99999
1.03	0.971027	1.01078	1.05506	1.06644	0.999966
1.04	0.961806	1.01433	1.07364	1.08902	0.999921
1.05	0.95279	1.01785	1.09232	1.11182	0.999848
1.06	0.943973	1.02135	1.11112	1.13484	0.999742
1.07	0.935349	1.02483	1.13001	1.15807	0.999598
1.08	0.926912	1.02829	1.14902	1.18153	0.999409
1.09	0.918655	1.03174	1.16813	1.2052	0.999172
1.1	0.910572	1.03517	1.18733	1.22909	0.998883
1.2	0.838274	1.06889	1.38462	1.48	0.992353
1.25	0.807099	1.08554	1.48649	1.61364	0.986137
1.3	0.778671	1.10217	1.59025	1.75273	0.977727
1.35	0.752651	1.11887	1.69571	1.89727	0.967067
1.4	0.728755	1.13569	1.80268	2.04727	0.954173
1.45	0.706742	1.15268	1.91097	2.20273	0.939113
1.5	0.686406	1.16988	2.02041	2.36364	0.922001
1.55	0.667572	1.18734	2.13082	2.53	0.902981
1.6	0.650085	1.20507	2.24204	2.70182	0.882221
1.65	0.633815	1.22311	2.3539	2.87909	0.859908
1.7	0.618643	1.24149	2.46625	3.06182	0.836236
1.75	0.604471	1.2602	2.57895	3.25	0.811406
1.8	0.591206	1.27929	2.69184	3.44364	0.785619
1.85	0.578771	1.29875	2.80481	3.64273	0.759072
1.9	0.567096	1.31859	2.91771	3.84727	0.731957
1.95	0.556116	1.33884	3.03043	4.05727	0.704456
2	0.545777	1.3595	3.14286	4.27273	0.67674
2.1	0.526823	1.40209	3.36641	4.72	0.621289
2.2	0.509888	1.4464	3.5876	5.18909	0.56672
2.3	0.49469	1.49248	3.80576	5.68	0.51393
2.4	0.480995	1.54036	4.0203	6.19273	0.463601
2.5	0.468609	1.59008	4.23077	6.72727	0.416218
2.6	0.457369	1.64166	4.43675	7.28364	0.372093
2.7	0.447136	1.69511	4.63794	7.86182	0.331388
2.8	0.437793	1.75045	4.83408	8.46182	0.294147
2.9	0.42924	1.80769	5.02499	9.08364	0.260322
3	0.421391	1.86685	5.21053	9.72727	0.229792
3.5	0.390381	2.1916	6.05618	13.2727	0.119782
4	0.368952	2.56508	6.76923	17.3636	0.0609583
4.5	0.353553	2.98765	7.36364	22	0.0309343
5	0.342136	3.4595	7.85714	27.1818	0.0158561
5.5	0.333448	3.98074	8.26708	32.9091	0.00827054
6	0.326693	4.55142	8.6087	39.1818	0.00440759
6.5	0.321342	5.1716	8.89474	46	0.00240442
7	0.317035	5.84129	9.13559	53.3636	0.00134336
7.5	0.313518	6.56051	9.33962	61.2727	0.000768493
8	0.310612	7.32929	9.51351	69.7273	0.000449813
8.5	0.308183	8.14762	9.66261	78.7273	0.000269117
9	0.306134	9.01551	9.79121	88.2727	0.000164394
9.5	0.304389	9.93297	9.90274	98.3636	0.000102414
10	0.302891	10.9	10	109	6.49931e-5
20	0.292292	40.6527	10.7317	436.273	9.66546e-8
25	0.290995	62.9668	10.8268	681.727	1.09381e-8
30	0.290288	90.2396	10.8791	981.727	1.81806e-9
35	0.289861	122.471	10.9109	1336.27	3.96e-10
40	0.289583	159.661	10.9317	1745.36	1.05364e-10
45	0.289393	201.81	10.9459	2209	3.26995e-11
50	0.289257	248.917	10.9562	2727.18	1.14652e-11
55	0.289156	300.983	10.9638	3299.91	4.4386e-12
60	0.289079	358.008	10.9695	3927.18	1.86519e-12
65	0.289019	419.992	10.974	4609	8.39774e-13
70	0.288972	486.934	10.9776	5345.36	4.01012e-13

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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