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Reflecting Shock (closed Valve) k =1.2

Isothermal Flow		Input: M		k = 1.2
M	fld	P/P*	P0/P0*	ρ/ρ*	U/U*
0.01	8323.31	91.2871	56.4759	91.2871	91.2871
0.02	2074.69	45.6435	28.243	45.6435	45.6435
0.03	918.095	30.429	18.8343	30.429	30.429
0.04	513.578	22.8218	14.1317	22.8218	22.8218
0.05	326.524	18.2574	11.3114	18.2574	18.2574
0.06	225.037	15.2145	9.43243	15.2145	15.2145
0.07	163.932	13.041	8.09124	13.041	13.041
0.08	124.339	11.4109	7.08621	11.4109	11.4109
0.09	97.2471	10.143	6.30528	10.143	10.143
0.1	77.9105	9.12871	5.68121	9.12871	9.12871
0.11	63.6383	8.29883	5.17125	8.29883	8.29883
0.12	52.8122	7.60726	4.74685	7.60726	7.60726
0.13	44.4115	7.02208	4.38827	7.02208	7.02208
0.14	37.7671	6.52051	4.08142	6.52051	6.52051
0.15	32.4251	6.08581	3.81594	6.08581	6.08581
0.16	28.0692	5.70544	3.58409	5.70544	5.70544
0.17	24.4735	5.36983	3.37993	5.36983	5.36983
0.18	21.4729	5.07151	3.19885	5.07151	5.07151
0.19	18.9449	4.80458	3.0372	4.80458	4.80458
0.2	16.7968	4.56435	2.89207	4.56435	4.56435
0.21	14.9575	4.347	2.76111	4.347	4.347
0.22	13.3717	4.14941	2.64238	4.14941	4.14941
0.23	11.996	3.969	2.53429	3.969	3.969
0.24	10.7957	3.80363	2.43552	3.80363	3.80363
0.25	9.74307	3.65148	2.34494	3.65148	3.65148
0.26	8.81559	3.51104	2.26162	3.51104	3.51104
0.27	7.99484	3.381	2.18474	3.381	3.381
0.28	7.26564	3.26025	2.11363	3.26025	3.26025
0.29	6.61541	3.14783	2.04768	3.14783	3.14783
0.3	6.03364	3.0429	1.98638	3.0429	3.0429
0.31	5.51148	2.94474	1.92929	2.94474	2.94474
0.32	5.04147	2.85272	1.87601	2.85272	2.85272
0.33	4.61728	2.76628	1.82619	2.76628	2.76628
0.34	4.23347	2.68491	1.77954	2.68491	2.68491
0.35	3.8854	2.6082	1.73578	2.6082	2.6082
0.36	3.56906	2.53575	1.69468	2.53575	2.53575
0.37	3.28099	2.46722	1.65602	2.46722	2.46722
0.38	3.01816	2.40229	1.61961	2.40229	2.40229
0.39	2.77796	2.34069	1.58529	2.34069	2.34069
0.4	2.55807	2.28218	1.55288	2.28218	2.28218
0.41	2.35649	2.22651	1.52227	2.22651	2.22651
0.42	2.17143	2.1735	1.49332	2.1735	2.1735
0.43	2.00132	2.12296	1.46592	2.12296	2.12296
0.44	1.84477	2.07471	1.43996	2.07471	2.07471
0.45	1.70053	2.0286	1.41535	2.0286	2.0286
0.46	1.56751	1.9845	1.39201	1.9845	1.9845
0.47	1.44472	1.94228	1.36985	1.94228	1.94228
0.48	1.33128	1.90181	1.34881	1.90181	1.90181
0.49	1.2264	1.863	1.32882	1.863	1.863
0.5	1.12936	1.82574	1.30981	1.82574	1.82574
0.51	1.03953	1.78994	1.29174	1.78994	1.78994
0.52	0.956323	1.75552	1.27455	1.75552	1.75552
0.53	0.87922	1.7224	1.25819	1.7224	1.7224
0.54	0.807745	1.6905	1.24263	1.6905	1.6905
0.55	0.741468	1.65977	1.22781	1.65977	1.65977
0.56	0.679997	1.63013	1.2137	1.63013	1.63013
0.57	0.622975	1.60153	1.20026	1.60153	1.60153
0.58	0.570077	1.57392	1.18748	1.57392	1.57392
0.59	0.521004	1.54724	1.1753	1.54724	1.54724
0.6	0.475485	1.52145	1.16371	1.52145	1.52145
0.61	0.43327	1.49651	1.15268	1.49651	1.49651
0.62	0.394131	1.47237	1.14218	1.47237	1.47237
0.63	0.357856	1.449	1.13219	1.449	1.449
0.64	0.324253	1.42636	1.12269	1.42636	1.42636
0.65	0.293142	1.40442	1.11367	1.40442	1.40442
0.66	0.264361	1.38314	1.10509	1.38314	1.38314
0.67	0.237756	1.36249	1.09695	1.36249	1.36249
0.68	0.213188	1.34246	1.08922	1.34246	1.34246
0.69	0.190527	1.323	1.0819	1.323	1.323
0.7	0.169652	1.3041	1.07496	1.3041	1.3041
0.71	0.150452	1.28573	1.06839	1.28573	1.28573
0.72	0.132824	1.26788	1.06219	1.26788	1.26788
0.73	0.116671	1.25051	1.05633	1.25051	1.25051
0.74	0.101903	1.23361	1.05082	1.23361	1.23361
0.75	0.0884389	1.21716	1.04562	1.21716	1.21716
0.76	0.0761995	1.20115	1.04075	1.20115	1.20115
0.77	0.0651129	1.18555	1.03618	1.18555	1.18555
0.78	0.0551117	1.17035	1.03191	1.17035	1.17035
0.79	0.046133	1.15553	1.02793	1.15553	1.15553
0.8	0.0381178	1.14109	1.02423	1.14109	1.14109
0.81	0.0310111	1.127	1.0208	1.127	1.127
0.82	0.0247613	1.11326	1.01764	1.11326	1.11326
0.83	0.0193203	1.09984	1.01474	1.09984	1.09984
0.84	0.0146427	1.08675	1.0121	1.08675	1.08675
0.85	0.0106862	1.07397	1.0097	1.07397	1.07397
0.86	0.00741095	1.06148	1.00755	1.06148	1.06148
0.87	0.0047795	1.04928	1.00563	1.04928	1.04928
0.88	0.00275674	1.03735	1.00395	1.03735	1.03735
0.89	0.00130964	1.0257	1.0025	1.0257	1.0257
0.9	0.00040711	1.0143	1.00126	1.0143	1.0143
0.91	1.98855e-5	1.00315	1.00025	1.00315	1.00315
0.910319	1.57028e-5	1.0028	1.00022	1.0028	1.0028
0.910638	1.20154e-5	1.00245	1.00019	1.00245	1.00245
0.910957	8.82253e-6	1.0021	1.00017	1.0021	1.0021
0.911276	6.12318e-6	1.00175	1.00014	1.00175	1.00175
0.911595	3.91655e-6	1.0014	1.00011	1.0014	1.0014
0.911914	2.20177e-6	1.00105	1.00008	1.00105	1.00105
0.912233	9.77996e-7	1.0007	1.00005	1.0007	1.0007
0.912552	2.44357e-7	1.00035	1.00003	1.00035	1.00035
0.912871	1.97215e-31	1	1	1	1

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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