yunplus/SuperFoil

Folder	Dataset	$(t\mathrm{/}c{)}_{\max }(t/c)\_\{\backslash max\}$	$M{a}_{\mathrm{\infty }}Ma\_\{\backslash infty\}$	$C_{L}C\_L$	$AoAAoA$(deg.)	$N_{\mathrm{A}\mathrm{i}\mathrm{r}\mathrm{f}\mathrm{o}\mathrm{i}\mathrm{l}\mathrm{s}}N\_\{\backslash mathrm\{Airfoils\}\}$	$N_{\mathrm{f}\mathrm{l}\mathrm{o}\mathrm{w}\mathrm{f}\mathrm{i}\mathrm{l}\mathrm{e}\mathrm{d}\mathrm{s}}N\_\{\backslash mathrm\{flowfileds\}\}$	Comment
FT	A-1	0.095	0.76	linspace(0.6, 1.0, 0.04)	/	1498	16478
	A-2	[0.113-0.124]	0.73	/	[-3.0 ~ 4.5]	501	27514	O-type grid
	A-3-t1	ls(0.09, 0.13, 0.01)	0.76	ls(0.6, 1.0, 0.04)	/	1414	15554	test dataset for A-1
VT/BUF	A-3-1 (n3)	ls(0.09, 0.13, 0.01)	ls(0.71, 0.76, 0.01)	/	[-3.0-5.0]	1217	25607	for buffet onset
VT/DD	A-3-2 (ma-n4; 8)	ls(0.09, 0.13, 0.01)	[0.65-0.80]	ls(0.6, 0.9, 0.01)	/	1266	17386	for drag divergence
VT/GU	A-3-3 (n5-2; 12)	U[0.085-0.135]	U[0.705-0.765]	[0.0-1.0]	/	1341	16031