Page 329 - Aeronautical Engineer Data Book

Appendix 5 267
Table A5.2 Continued
Weak solution
M 1
M 2 P 2 /P 1
1.20 0.0 56.44 1.200 1.000
1.20 1.0 58.55 1.158 1.056
1.20 2.0 61.05 1.111 1.120
1.20 3.0 64.34 1.056 1.198
1.25 0.0 53.13 1.25 1.000
1.25 1.0 54.88 1.211 1.053
1.25 2.0 56.85 1.170 1.111
1.25 3.0 59.13 1.124 1.176
1.25 4.0 61.99 1.072 1.254
1.25 5.0 66.59 0.999 1.366
1.30 0.0 50.29 1.300 1.000
1.30 1.0 51.81 1.263 1.051
1.30 2.0 53.48 1.224 1.107
1.30 3.0 55.32 1.184 1.167
1.30 4.0 57.42 1.140 1.233
1.30 5.0 59.96 1.090 1.311
1.30 6.0 63.46 1.027 1.411
1.35 0.0 47.80 1.350 1.000
1.35 1.0 49.17 1.314 1.051
1.35 2.0 50.64 1.277 1.104
1.35 3.0 52.22 1.239 1.162
1.35 4.0 53.97 1.199 1.224
1.35 5.0 55.93 1.157 1.292
1.35 6.0 58.23 1.109 1.370
1.35 7.0 61.18 1.052 1.466
1.35 8.0 66.92 0.954 1.633
1.40 0.0 45.59 1.400 1.000
1.40 1.0 46.84 1.365 1.050
1.40 2.0 48.17 1.330 1.103
1.40 3.0 49.59 1.293 1.159
1.40 4.0 51.12 1.255 1.219
1.40 5.0 52.78 1.216 1.283
1.40 6.0 54.63 1.174 1.354
1.40 7.0 56.76 1.128 1.433
1.40 8.0 59.37 1.074 1.526
1.40 9.0 63.19 1.003 1.655
2.20 0.0 27.04 2.200 1.000
2.20 2.0 28.59 2.124 1.127
2.20 4.0 30.24 2.049 1.265
2.20 6.0 31.98 1.974 1.417
2.20 8.0 33.83 1.899 1.583
2.20 10.0 35.79 1.823 1.764
2.20 12.0 37.87 1.745 1.961
2.20 14.0 40.10 1.666 2.176
2.20 16.0 42.49 1.583 2.410
2.20 18.0 45.09 1.496 2.666
2.20 20.0 47.98 1.404 2.949
2.20 22.0 51.28 1.301 3.270
2.20 24.0 55.36 1.181 3.655
2.20 26.0 62.70 0.980 4.292