########################################################################### # #TA1 Comparison of 2D experimental and CFD results # #File contains wake/boundary layer data from the RANSMB CFD solution. It #comprises distance traversed normal to the wing surface and Cptotal. # # #Free stream Velocity :67 ms-1 #Reynolds number :3.52E6 #Mach number :0.197 #Mode :Pitch #Angle of Attack :4.01 deg #Wing chord (retracted) :0.7635m # #Boundary layer taken at location 0.899C wing chord relative to the retracted #wing chord value. ########################################################################### %AC= %Column1Name= Distance traversed normal to the surface %Column1Units= Non-dimensional %Column1Type= Real %Column2Name= Coefficient of Total pressure %Column2Units= Non-dimensional %Column2Type= Real %End Of Metadata 0.1103161 0.9879601 0.1049135 0.9883220 0.1011185 0.9885787 0.0948539 0.9897436 0.0905921 0.9912144 0.0875395 0.9931216 0.0845879 0.9949426 0.0817332 0.9967595 0.0789706 0.9978792 0.0762970 0.9976357 0.0737086 0.9949933 0.0712016 0.9889602 0.0687717 0.9787069 0.0663770 0.9639353 0.0657635 0.9591467 0.0639773 0.9451798 0.0616881 0.9236954 0.0595818 0.9009993 0.0577072 0.8787437 0.0560875 0.8582655 0.0547236 0.8405030 0.0535997 0.8258886 0.0526899 0.8144267 0.0519641 0.8058298 0.0513918 0.7996550 0.0509445 0.7953845 0.0505975 0.7925460 0.0503298 0.7907175 0.0501241 0.7895723 0.0499666 0.7888673 0.0498464 0.7884450 0.0497547 0.7881898 0.0496849 0.7880400 0.0496318 0.7879548 0.0495915 0.7879009 0.0495609 0.7878760 0.0495377 0.7878691 0.0495201 0.7878686 0.0495067 0.7878774 0.0494966 0.7878881 0.0494889 0.7879076 0.0494831 0.7879362 0.0494787 0.7879680 0.0494743 0.7879959 0.0494699 0.7880441 0.0494654 0.7881294 0.0494611 0.7882360 0.0494568 0.7882957 0.0494525 0.7883321 0.0494481 0.7883638 0.0494428 0.7883868 0.0494363 0.7884154 0.0494283 0.7884371 0.0494185 0.7884530 0.0494064 0.7884769 0.0493916 0.7884970 0.0493734 0.7885191 0.0493510 0.7885417 0.0493234 0.7885769 0.0492894 0.7886266 0.0492474 0.7886994 0.0491955 0.7888170 0.0491312 0.7889985 0.0490513 0.7892905 0.0489518 0.7897639 0.0488272 0.7905306 0.0486706 0.7917961 0.0484726 0.7938536 0.0482200 0.7971833 0.0478948 0.8022390 0.0474706 0.8094946 0.0469077 0.8183205 0.0461439 0.8267036 0.0450752 0.8283525 0.0435139 0.8138781 0.0410810 0.7688225 0.0368799 0.6848440 0.0326635 0.5597160 0.0285331 0.4055651 0.0245810 0.2531606 0.0223996 0.1115468 0.0210340 -0.0026256 0.0201107 -0.0802168 0.0194534 -0.1266353 0.0189681 -0.1410308 0.0186002 -0.1301423 0.0183155 -0.0987471 0.0180918 -0.0540805 0.0179138 -0.0014623 0.0177709 0.0537850 0.0176551 0.1081791 0.0175609 0.1591607 0.0174837 0.2054545 0.0174202 0.2463796 0.0173679 0.2818565 0.0173246 0.3120938 0.0172886 0.3375538 0.0172588 0.3587752 0.0172339 0.3763590 0.0172132 0.3908484 0.0171959 0.4027694 0.0171815 0.4125754 0.0171694 0.4206545 0.0171593 0.4273305 0.0171509 0.4328469 0.0171438 0.4375777 0.0171379 0.4416347 0.0171320 0.4453910 0.0171261 0.4492698 0.0171202 0.4534092 0.0171148 0.4572028 0.0171094 0.4606269 0.0171041 0.4640394 0.0170987 0.4674653 0.0170924 0.4711863 0.0170850 0.4755798 0.0170762 0.4806550 0.0170659 0.4865420 0.0170537 0.4933379 0.0170392 0.5010935 0.0170222 0.5098220 0.0170020 0.5194188 0.0169780 0.5296856 0.0169495 0.5403306 0.0169156 0.5510447 0.0168750 0.5615624 0.0168264 0.5717071 0.0167679 0.5813988 0.0166972 0.5907018 0.0166113 0.5996668 0.0165062 0.6086074 0.0163764 0.6174924 0.0162146 0.6272253 0.0160101 0.6371587 0.0157474 0.6500702 0.0154030 0.6632447 0.0149386 0.6849309 0.0142890 0.7069700 0.0133329 0.7499635 0.0120897 0.7845553 0.0118173 0.7935794 0.0091035 0.8533712 0.0073500 0.8982200 0.0063481 0.9235620 0.0035284 0.9584680 0.0017236 0.9707452 0.0006590 0.9764777 -0.0020530 0.9731379 -0.0037907 0.9673655 -0.0045192 0.9652991 -0.0067948 0.9582968 -0.0083843 0.9596362 -0.0087723 0.9592809 -0.0106240 0.9611131 -0.0120299 0.9698554 -0.0121582 0.9698402 -0.0136980 0.9737146 -0.0145524 0.9813216 -0.0149961 0.9816052 -0.0161836 0.9892426 -0.0164507 0.9925873 -0.0176991 0.9940573 -0.0179045 0.9962376 -0.0190974 1.0007440 -0.0196859 0.9970315 -0.0201653 0.9985025