PW98-mod (pw98mod-pw) Xfoil prediction polar at RE=5,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: PW98-mod (pw98mod-pw) Reynolds number: 5,000,000 Max Cl/Cd: 106.82 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-pw98mod-pw-5000000.txt Download as CSV file: xf-pw98mod-pw-5000000.csv |
XFOIL Version 6.96
Calculated polar for: PW98-mod
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 5.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.500 -0.8121 0.02376 0.02189 -0.0102 1.0000 0.0006
-8.250 -0.7979 0.01925 0.01695 -0.0095 0.9965 0.0006
-8.000 -0.7808 0.01644 0.01377 -0.0082 0.9614 0.0006
-7.750 -0.7622 0.01438 0.01137 -0.0067 0.9372 0.0006
-7.500 -0.7403 0.01269 0.00938 -0.0057 0.9156 0.0006
-7.250 -0.7166 0.01132 0.00773 -0.0050 0.8949 0.0006
-7.000 -0.6931 0.00966 0.00570 -0.0041 0.8737 0.0007
-6.750 -0.6677 0.00865 0.00435 -0.0035 0.8519 0.0009
-6.500 -0.6404 0.00826 0.00378 -0.0033 0.8309 0.0010
-6.250 -0.6126 0.00802 0.00341 -0.0031 0.8092 0.0012
-6.000 -0.5846 0.00785 0.00313 -0.0030 0.7874 0.0013
-3.500 -0.2968 0.01025 0.00564 -0.0048 0.5992 0.0023
-3.250 -0.2690 0.00970 0.00501 -0.0046 0.5845 0.0012
-3.000 -0.2410 0.00929 0.00454 -0.0045 0.5701 0.0011
-2.750 -0.2130 0.00888 0.00408 -0.0044 0.5556 0.0010
-2.500 -0.1851 0.00845 0.00358 -0.0043 0.5417 0.0010
-2.250 -0.1572 0.00801 0.00308 -0.0041 0.5277 0.0009
-2.000 -0.1293 0.00759 0.00260 -0.0039 0.5139 0.0009
-1.750 -0.1014 0.00716 0.00210 -0.0037 0.5001 0.0009
-1.500 -0.0733 0.00684 0.00169 -0.0036 0.4853 0.0010
-1.250 -0.0443 0.00730 0.00205 -0.0041 0.4692 0.0019
-1.000 -0.0164 0.00612 0.00064 -0.0031 0.4562 0.0055
-0.750 0.0122 0.00610 0.00061 -0.0032 0.4425 0.0065
-0.500 0.0408 0.00609 0.00057 -0.0033 0.4287 0.0072
-0.250 0.0694 0.00608 0.00053 -0.0034 0.4147 0.0083
0.000 0.0980 0.00608 0.00051 -0.0035 0.4010 0.0086
0.250 0.1267 0.00610 0.00051 -0.0035 0.3867 0.0122
0.500 0.1553 0.00612 0.00051 -0.0036 0.3731 0.0157
0.750 0.1839 0.00613 0.00051 -0.0037 0.3588 0.0201
1.000 0.2120 0.00595 0.00050 -0.0038 0.3459 0.1040
1.250 0.2395 0.00556 0.00050 -0.0040 0.3319 0.2794
1.500 0.2648 0.00465 0.00051 -0.0040 0.3191 0.6447
1.750 0.2903 0.00418 0.00055 -0.0036 0.3061 0.8369
2.000 0.3176 0.00413 0.00059 -0.0034 0.2946 0.8856
2.250 0.3445 0.00412 0.00064 -0.0031 0.2818 0.9208
2.500 0.3713 0.00416 0.00069 -0.0027 0.2700 0.9445
2.750 0.3967 0.00445 0.00082 -0.0023 0.2140 0.9685
3.000 0.4247 0.00491 0.00100 -0.0025 0.1431 0.9839
3.250 0.4540 0.00589 0.00146 -0.0033 0.0101 0.9931
3.500 0.4892 0.00607 0.00159 -0.0050 0.0021 0.9965
3.750 0.5230 0.00618 0.00168 -0.0063 0.0008 0.9986
4.000 0.5555 0.00631 0.00179 -0.0074 0.0007 0.9997
4.250 0.5838 0.00644 0.00191 -0.0075 0.0008 1.0000
4.500 0.6103 0.00657 0.00201 -0.0072 0.0008 1.0000
4.750 0.6369 0.00669 0.00210 -0.0070 0.0009 1.0000
5.000 0.6637 0.00682 0.00220 -0.0068 0.0011 1.0000
5.250 0.6910 0.00684 0.00221 -0.0067 0.0086 1.0000
5.500 0.7189 0.00673 0.00218 -0.0066 0.0258 1.0000
5.750 0.7454 0.00718 0.00252 -0.0065 0.0049 1.0000
6.000 0.7729 0.00734 0.00265 -0.0064 0.0023 1.0000
6.500 0.8272 0.00787 0.00324 -0.0063 0.0012 1.0000
6.750 0.8545 0.00811 0.00350 -0.0063 0.0009 1.0000
7.000 0.8815 0.00844 0.00388 -0.0062 0.0007 1.0000
|
Polar data table (+)
Polar graphs
<< Back to PW98-mod (pw98mod-pw)