Page 316 - Aeronautical Engineer Data Book

254 Aeronautical Engineer’s Data Book
Table A4.1 Continued
M P/P o / o T/T o q/P o A/A* V/a*

0.31 0.9355 0.9535 0.9811 0.9507 6.293e–2 1.9765 0.3364
0.32 0.9315 0.9506 0.9799 0.9474 6.677e–2 1.9219 0.3470
0.33 0.9274 0.9476 0.9787 0.9440 7.069e–2 1.8707 0.3576
0.34 0.9231 0.9445 0.9774 0.9404 7.470e–2 1.8229 0.3682
0.35 0.9188 0.9413 0.9761 0.9367 7.878e–2 1.7780 0.3788
0.36 0.9143 0.9380 0.9747 0.9330 8.295e–2 1.7358 0.3893
0.37 0.9098 0.9347 0.9733 0.9290 8.719e–2 1.6961 0.3999
0.38 0.9052 0.9313 0.9719 0.9250 9.149e–2 1.6587 0.4104
0.39 0.9004 0.9278 0.9705 0.9208 9.587e–2 1.6234 0.4209
0.40 0.8956 0.9243 0.9690 0.9165 0.1003 1.5901 0.4313
0.41 0.8907 0.9207 0.9675 0.9121 0.1048 1.5587 0.4418
0.42 0.8857 0.9170 0.9659 0.9075 0.1094 1.5289 0.4522
0.43 0.8807 0.9132 0.9643 0.9028 0.1140 1.5007 0.4626
0.44 0.8755 0.9094 0.9627 0.8980 0.1186 1.4740 0.4729
0.45 0.8703 0.9055 0.9611 0.8930 0.1234 1.4487 0.4833
0.46 0.8650 0.9016 0.9594 0.8879 0.1281 1.4246 0.4936
0.47 0.8596 0.8976 0.9577 0.8827 0.1329 1.4018 0.5038
0.48 0.8541 0.8935 0.9559 0.8773 0.1378 1.3801 0.5141
0.49 0.8486 0.8894 0.9542 0.8717 0.1426 1.3595 0.5243
0.50 0.8430 0.8852 0.9524 0.8660 0.1475 1.3398 0.5345
0.51 0.8374 0.8809 0.9506 0.8602 0.1525 1.3212 0.5447
0.52 0.8317 0.8766 0.9487 0.8542 0.1574 1.3034 0.5548
0.53 0.8259 0.8723 0.9468 0.8480 0.1624 1.2865 0.5649
0.54 0.8201 0.8679 0.9449 0.8417 0.1674 1.2703 0.5750
0.55 0.8142 0.8634 0.9430 0.8352 0.1724 1.2549 0.5851
0.56 0.8082 0.8589 0.9410 0.8285 0.1774 1.2403 0.5951
0.57 0.8022 0.8544 0.9390 0.8216 0.1825 1.2263 0.6051
0.58 0.7962 0.8498 0.9370 0.8146 0.1875 1.2130 0.6150
0.59 0.7901 0.8451 0.9349 0.8074 0.1925 1.2003 0.6249
0.60 0.7840 0.8405 0.9328 0.8000 0.1976 1.1882 0.6348
0.61 0.7778 0.8357 0.9307 0.7924 0.2026 1.1767 0.6447
0.62 0.7716 0.8310 0.9286 0.7846 0.2076 1.1656 0.6545
0.63 0.7654 0.8262 0.9265 0.7766 0.2127 1.1552 0.6643
0.64 0.7591 0.8213 0.9243 0.7684 0.2177 1.1451 0.6740
0.65 0.7528 0.8164 0.9221 0.7599 0.2226 1.1356 0.6837
0.66 0.7465 0.8115 0.9199 0.7513 0.2276 1.1265 0.6934
0.67 0.7401 0.8066 0.9176 0.7424 0.2326 1.1179 0.7031
0.68 0.7338 0.8016 0.9153 0.7332 0.2375 1.1097 0.7127
0.69 0.7274 0.7966 0.9131 0.7238 0.2424 1.1018 0.7223
0.70 0.7209 0.7916 0.9107 0.7141 0.2473 1.0944 0.7318
0.71 0.7145 0.7865 0.9084 0.7042 0.2521 1.0873 0.7413
0.72 0.7080 0.7814 0.9061 0.6940 0.2569 1.0806 0.7508
0.73 0.7016 0.7763 0.9037 0.6834 0.2617 1.0742 0.7602
0.74 0.6951 0.7712 0.9013 0.6726 0.2664 1.0681 0.7696
0.75 0.6886 0.7660 0.8989 0.6614 0.2711 1.0624 0.7789
0.76 0.6821 0.7609 0.8964 0.6499 0.2758 1.0570 0.7883
0.77 0.6756 0.7557 0.8940 0.6380 0.2804 1.0519 0.7975
0.78 0.6691 0.7505 0.8915 0.6258 0.2849 1.0471 0.8068
0.79 0.6625 0.7452 0.8890 0.6131 0.2894 1.0425 0.8160
0.80 0.6560 0.7400 0.8865 0.6000 0.2939 1.0382 0.8251
0.81 0.6495 0.7347 0.8840 0.5864 0.2983 1.0342 0.8343
0.82 0.6430 0.7295 0.8815 0.5724 0.3026 1.0305 0.8433
0.83 0.6365 0.7242 0.8789 0.5578 0.3069 1.0270 0.8524
0.84 0.6300 0.7189 0.8763 0.5426 0.3112 1.0237 0.8614
0.85 0.6235 0.7136 0.8737 0.5268 0.3153 1.0207 0.8704
0.86 0.6170 0.7083 0.8711 0.5103 0.3195 1.0179 0.8793