[讨论]Onera M6

xthang

各位尊敬的同僚:
    本人近期做了个用于计算三维任意速度粘性流的程序,跨音速算例采用Onera M6三维机翼,但结果跟实验数据有点差别,本人怀疑是我的机翼几何数据不对,因此特地来这里向大家求助,哪位手头有Onera M6机翼数据的,请给我一份,本人不胜感激,期待与各位广泛交流经验.

xthang

我的邮箱:  xthang@tom.com   ,请大家帮忙

boling2000

这是翼型数据，自己对比一下
0.0000000  0.0000000
0.0000165  0.0006914
0.0000696  0.0014416
0.0001675  0.0022554
0.0003232  0.0031382
0.0005508  0.0040959
0.0008657  0.0051343
0.0012868  0.0062598
0.0018364  0.0074784
0.0025441  0.0087958
0.0034428  0.0102163
0.0045704  0.0117419
0.0059751  0.0133708
0.0077112  0.0150951
0.0098413  0.0168984
0.0124479  0.0187537
0.0156171  0.0206220
0.0194609  0.0224545
0.0241067  0.0242004
0.0297008  0.0258245
0.0364261  0.0273317
0.0444852  0.0287912
0.0541248  0.0303278
0.0656303  0.0320138
0.0793366  0.0338372
0.0956354  0.0357742
0.1149796  0.0377923
0.1378963  0.0398522
0.1649976  0.0419089
0.1919327  0.0436214
0.2187096  0.0450507
0.2453310  0.0462358
0.2717978  0.0471987
0.2981113  0.0479494
0.3242726  0.0484902
0.3502830  0.0488183
0.3761446  0.0489296
0.4018567  0.0488202
0.4274223  0.0484833
0.4528441  0.0479351
0.4781197  0.0471661
0.5032514  0.0461903
0.5282426  0.0450209
0.5530937  0.0436741
0.5778043  0.0421684
0.6023757  0.0405241
0.6268104  0.0387613
0.6511093  0.0368990
0.6752726  0.0349542
0.6993027  0.0329402
0.7231995  0.0308662
0.7469658  0.0287365
0.7705998  0.0265505
0.7941055  0.0243027
0.8174828  0.0219842
0.8407324  0.0195838
0.8638564  0.0170915
0.8868235  0.0145051
0.9061905  0.0122389
0.9225336  0.0102727
0.9363346  0.0085827
0.9479946  0.0071423
0.9578511  0.0059224
0.9661860  0.0048907
0.9732361  0.0040180
0.9792020  0.0032796
0.9842508  0.0026547
0.9885252  0.0021257
0.9921438  0.0016778
0.9952080  0.0012985
0.9978030  0.0009773
1.0000000  0.0007052

xthang

我用的就是这个数据，可能还是我的程序有点问题，不过还是要多谢boling2000 的支持。多谢！

lyxliuti

谢谢二楼，我也需要

dajiangyou_v5

新手学习了