Conceptual Aircraft Design

Appendix BInternational Standard Atmosphere Table Data from Hydrostatic Equations

Altitude (m)	Pressure (N/m2)	Temperature (K)	Density (kg/m3)	Viscosity (Ns/m2)	Sound speed (m/s)	Cf_turbulent
0	101327	288.15	1.225	0.00001789	340.3	0.00263
500	95463	284.9	1.16727	0.00001773	338.37	0.00264
1000	89876.7	281.65	1.11164	0.00001757	336.44	0.00266
1500	84558	278.4	1.05807	0.00001741	334.49	0.00267
2000	79497.2	275.15	1.00649	0.00001725	332.53	0.00269
2500	74684.4	271.9	0.95686	0.00001709	330.56	0.00271
3000	70110.4	268.65	0.90912	0.0001693	328.58	0.00273
3500	65765.8	265.4	0.86323	0.00001677	326.59	0.00274
4000	61641.9	262.15	0.81913	0.00001661	324.58	0.00276
4500	57729.9	258.9	0.77678	0.00001644	322.56	0.00278
5000	54021.5	255.65	0.73612	0.00001628	320.53	0.0028
5500	50508.3	252.4	0.69711	0.00001611	318.49	0.00282
6000	47182.5	249.15	0.6597	0.00001594	316.43	0.00284
6500	44036.2	245.9	0.62385	0.00001577	314.36	0.00286
7000	41062.1	242.65	0.5895	0.0000156	312.28	0.00288
7500	38252.7	239.4	0.55663	0.00001543	310.18	0.0029
8000	35601	236.15	0.52517	0.00001526	308.07	0.00292
8500	33100.2	232.9	0.49509	0.00001509	305.94	0.00294
9000	30743.6	229.65	0.46635	0.00001492	303.8	0.00297
9500	28524.7	226.4	0.4389	0.00001474	301.64	0.00299
10000	26437.3	223.15	0.41271	0.00001457	299.47	0.00301
10500	24475.3	219.9	0.38773	0.00001439	297.28	0.00304
11000	22633	216.65	0.36392	0.00001421	295.07	0.00306
11500	20916.8	216.65	0.33633	0.00001421	295.07 ...