Page 318 - Aeronautical Engineer Data Book

256 Aeronautical Engineer’s Data Book
Table A4.2 Continued

M P/P o / o T/T o q/P o A/A* V/a*
1.23 0.3964 0.5164 0.7677 0.7162 0.4198 1.0398 1.1806
1.24 0.3912 0.5115 0.7648 0.7332 0.4211 1.0432 1.1879
1.25 0.3861 0.5067 0.7619 0.7500 0.4223 1.0468 1.1952
1.26 0.3809 0.5019 0.7590 0.7666 0.4233 1.0504 1.2025
1.27 0.3759 0.4971 0.7561 0.7829 0.4244 1.0542 1.2097
1.28 0.3708 0.4923 0.7532 0.7990 0.4253 1.0581 1.2169
1.29 0.3658 0.4876 0.7503 0.8149 0.4262 1.0621 1.2240
1.30 0.3609 0.4829 0.7474 0.8307 0.4270 1.0663 1.2311
1.31 0.3560 0.4782 0.7445 0.8462 0.4277 1.0706 1.2382
1.32 0.3512 0.4736 0.7416 0.8616 0.4283 1.0750 1.2452
1.33 0.3464 0.4690 0.7387 0.8769 0.4289 1.0796 1.2522
1.34 0.3417 0.4644 0.7358 0.8920 0.4294 1.0842 1.2591
1.35 0.3370 0.4598 0.7329 0.9069 0.4299 1.0890 1.2660
1.36 0.3323 0.4553 0.7300 0.9217 0.4303 1.0940 1.2729
1.37 0.3277 0.4508 0.7271 0.9364 0.4306 1.0990 1.2797
1.38 0.3232 0.4463 0.7242 0.9510 0.4308 1.1042 1.2864
1.39 0.3187 0.4418 0.7213 0.9655 0.4310 1.1095 1.2932
1.40 0.3142 0.4374 0.7184 0.9798 0.4311 1.1149 1.2999
1.41 0.3098 0.4330 0.7155 0.9940 0.4312 1.1205 1.3065
1.42 0.3055 0.4287 0.7126 1.0082 0.4312 1.1262 1.3131
1.43 0.3012 0.4244 0.7097 1.0222 0.4311 1.1320 1.3197
1.44 0.2969 0.4201 0.7069 1.0361 0.4310 1.1379 1.3262
1.45 0.2927 0.4158 0.7040 1.0500 0.4308 1.1440 1.3327
1.46 0.2886 0.4116 0.7011 1.0638 0.4306 1.1501 1.3392
1.47 0.2845 0.4074 0.6982 1.0775 0.4303 1.1565 1.3456
1.48 0.2804 0.4032 0.6954 1.0911 0.4299 1.1629 1.3520
1.49 0.2764 0.3991 0.6925 1.1046 0.4295 1.1695 1.3583
1.50 0.2724 0.3950 0.6897 1.1180 0.4290 1.1762 1.3646
1.51 0.2685 0.3909 0.6868 1.1314 0.4285 1.1830 1.3708
1.52 0.2646 0.3869 0.6840 1.1447 0.4279 1.1899 1.3770
1.53 0.2608 0.3829 0.6811 1.1580 0.4273 1.1970 1.3832
1.54 0.2570 0.3789 0.6783 1.1712 0.4266 1.2042 1.3894
1.55 0.2533 0.3750 0.6754 1.1843 0.4259 1.2116 1.3955
1.56 0.2496 0.3710 0.6726 1.1973 0.4252 1.2190 1.4015
1.57 0.2459 0.3672 0.6698 1.2103 0.4243 1.2266 1.4075
1.58 0.2423 0.3633 0.6670 1.2233 0.4235 1.2344 1.4135
1.59 0.2388 0.3595 0.6642 1.2362 0.4226 1.2422 1.4195
1.60 0.2353 0.3557 0.6614 1.2490 0.4216 1.2502 1.4254
1.61 0.2318 0.3520 0.6586 1.2618 0.4206 1.2584 1.4313
1.62 0.2284 0.3483 0.6558 1.2745 0.4196 1.2666 1.4371
1.63 0.2250 0.3446 0.6530 1.2872 0.4185 1.2750 1.4429
1.64 0.2217 0.3409 0.6502 1.2998 0.4174 1.2836 1.4487
1.65 0.2184 0.3373 0.6475 1.3124 0.4162 1.2922 1.4544
1.66 0.2151 0.3337 0.6447 1.3250 0.4150 1.3010 1.4601
1.67 0.2119 0.3302 0.6419 1.3375 0.4138 1.3100 1.4657
1.68 0.2088 0.3266 0.6392 1.3500 0.4125 1.3190 1.4713
1.69 0.2057 0.3232 0.6364 1.3624 0.4112 1.3283 1.4769
1.70 0.2026 0.3197 0.6337 1.3748 0.4098 1.3376 1.4825
1.71 0.1996 0.3163 0.6310 1.3871 0.4085 1.3471 1.4880
1.72 0.1966 0.3129 0.6283 1.3994 0.4071 1.3567 1.4935
1.73 0.1936 0.3095 0.6256 1.4117 0.4056 1.3665 1.4989
1.74 0.1907 0.3062 0.6229 1.4239 0.4041 1.3764 1.5043
1.75 0.1878 0.3029 0.6202 1.4361 0.4026 1.3865 1.5097
1.76 0.1850 0.2996 0.6175 1.4483 0.4011 1.3967 1.5150
1.77 0.1822 0.2964 0.6148 1.4604 0.3996 1.4070 1.5203
1.78 0.1794 0.2931 0.6121 1.4725 0.3980 1.4175 1.5256