Normal Shock Table for Air (k=1.4)
	1.00	1.00000	1.0000	1.0000	1.0000	1.00000	1.8929
	1.10	0.91177	1.2450	1.1691	1.0649	0.99892	2.1328
	1.20	0.84217	1.5133	1.3416	1.1280	0.99280	2.4075
	1.30	0.78596	1.8050	1.5157	1.1909	0.97935	2.7135
	1.40	0.73971	2.1200	1.6896	1.2547	0.95819	3.0493
	1.50	0.70109	2.4583	1.8621	1.3202	0.92978	3.4133
	1.60	0.66844	2.8201	2.0317	1.3880	0.89520	3.8049
	1.70	0.64055	3.2050	2.1977	1.4583	0.85573	4.2238
	1.80	0.61650	3.6133	2.3592	1.5316	0.81268	4.6695
	1.90	0.59562	4.0450	2.5157	1.6079	0.76735	5.1417
	2.00	0.57735	4.5000	2.6666	1.6875	0.72088	5.6405
	2.10	0.56128	4.9784	2.8119	1.7704	0.67422	6.1655
	2.20	0.54706	5.4800	2.9512	1.8569	0.62812	6.7163
	2.30	0.53441	6.0050	3.0846	1.9468	0.58331	7.2937
	2.40	0.52312	6.5533	3.2119	2.0403	0.54015	7.8969
	2.50	0.51299	7.1250	3.3333	2.1375	0.49902	8.5262
	2.60	0.50387	7.7200	3.4489	2.2383	0.46012	9.1813
	2.70	0.49563	8.3383	3.5590	2.3429	0.42359	9.8625
	2.80	0.48817	8.9800	3.6635	2.4512	0.38946	10.569
	2.90	0.48138	9.6450	3.7629	2.5632	0.35773	11.302
	3.00	0.47519	10.333	3.8571	2.6790	0.32834	12.061
	4.00	0.43496	18.500	4.5714	4.0469	0.13876	21.068
	5.00	0.41523	29.000	5.0000	5.8000	0.06172	32.654
	10.00	0.38757	116.50	5.7143	20.388	0.00304	129.217
	∞	0.37796	∞	6.000	∞	0	∞