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TABLE XI.--NORMALIZED SHROUD STATIC PRESSURES FOR A RANGE OF MASS FLOW RATES m/m S, percent 38.45 51.34 NORMALIZED SHROUD STATIC PRESSURE, P/Pstd rh/rh a, percent 57.08 62.45 68.04 76.01 83.37 90.22 99.94 115.93 132.40 -500.0 1.(_K_9o1.ooooo 1.o_xJ i.oooo3 I.OO(_I 1.ooooo I.OOo._oi.ooooo I._ -487.0 l.O(Xq09 1.00010 1.(_010 1.09009 0.99659 0.99591 0.995011 0.99393 0.99428 0.99271 0.99352 0.99257 0.99.369 0.99206 0.99376 0.99204 0.99403 0.99233 0.99507 0.99284 1.00026 0.99967 1.00895 !.01000 1.018116 1.01922 1.03462 1.03538 1.060311 1.06060 1.08837 1.08878 1,10326 1.10372 |.111_7 1.11120 1.11625 1.11688 1.12027 1.12130 1.12060 1.12168 1.12167 1.12289 1.12214 1.12320 1.12295 1.12401 1.12397 1.12517 1.13054 1.12942 1.01KI05 1.00012 1.00006 1.00007 1.ooooo i.ooooo 1.00010 i.0010 0.99989 0.98944 0.98573 0.98129 0.98429 io.97878 0.97221 -38.9 0.99846 0.99724 0.99514 0.99392 0.99271 0.99097 0.99107 0.98879 0.98973 0.98710 0.98997 0.98730 0.98989 0.98711 0.99012 0.98713 0.99067 0.98724 0.99771 0.99237 1.00632 0.99962 1.01600 1.00976 1.03265 1.02700 1.058111 1.05270 1.08693 1.08210 1,10194 1.09766 1.10939 1.111527 1.11490 1.11054 1.11932 1.11487 1.11978 1.11537 1.12106 1.11672 1.12132 1.11689 1.12213 1.11777 1,12364 1.11951 1.12765 1.12300 0.9926810.99141 0.98909 0.98721 0.98653 0.98422 111.98492 0.98273 0.98465 0.98195 0.98514 0.98362 0.98409 0,98087 0.98417 0.98012 0.98574 0.98066 10.99269 0.98563 1.00323 0.99639 ]1.02134 1.01622 1.04785 1.04295 1.07658 1.07080 1,09275J 1.118751 1.10105_ 1.09634 1.10571 IA0069 1.11010 I 1.10472 1.11064 1.10525 _1.11196 1.10663 1.11184 1.10665 1.11273 1.10754 1.11468 1.10954 1.11791 1.11226i -28.1 0.99819 0.99598 -9.7 0.99826 -4.9 0.99826 -2.4 1.011069 -I.2 1.00108 0.0 1.00138 2.0 1.00235 5.0 i.00395 15.1 1.00792 30.1 1.01556 50.0 1.03369 69.9 1.06031 86.6 1.08765 95.0 1.10257 100.0 1.11020 104.9 1.11556 109.7 1.11894 111.3 1.11951 114.6 1.12124 117.11 1.12290 119.4 1.12456 121,8 1.12599 274.7 1.13576 0.99523 0.99489 0.99586 0.99604 0.99626 0.99707 1.00131 1.00926 1.01800 1.03479 1.06066 1.08836 1,10343 1.11115 I.II676 1.12080 1.12135 1.12291 1.12390 1.12534 1.12694 1.13393 ; 0.98066 0.97884 0.97878 0.98114 0.97586 0.97547 0.97560 0.97666 0.98587 1.00842 1.03523 1.06400 1,08011 1.08948 1.09303 1.09665 1.09742 1.09908 1.09983 1.10099 1.10268 1.111514 0.97392 0.%592 0.97170,0.96294 0.96978 0.96046 0.96867 0,95874 0.96607 0.954(}9 0.95985 0.94173 0.95692'0.93565 0.95545 0.93429 0.96594[0.94136 0.99142 0.96971 1.0188310.99877 1.04981 1.03174 1,06665 1.04932 1.07659 1.115%3 1.07960 1.06271 1.08206 1.06479 1.08262 1.06514 1.08389 1.06612 1.08512 1.06652 1.08641 1.06736 1.08745 1.06845 1.09251 1.07396 i I i [ I 35PDF Image | Laser anemometer measurements of the three-dimensional rotor flow
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