资 源 简 介
一个可以生成标准翼型坐标，并对翼型在不同攻角下进行升力系数及阻力系数计算的软件。-Can generate a standard airfoil coordinates, and the airfoil at different angle of attack carried out under the lift coefficient and drag coefficient calculation software.
文 件 列 表
pablo
CAST7.DAT
cfturb.m
CLARKY.DAT
close_te.m
DAE11.DAT
DAE21.DAT
DAE31.DAT
dist.m
doublet.m
DSMA523.DAT
ellipse.m
EPP662.DAT
EPP748.DAT
fH.m
findy.m
fL.m
FOIL31.DAT
FX63137.DAT
GAW1.DAT
H1ofH.m
HofH1.m
HSN0213.DAT
info.m
K720616.DAT
K790312.DAT
K820609.DAT
KORN.DAT
library.m
LISS7769.DAT
LS10013.DAT
LS10417M.DAT
MS10313.DAT
MS10317.DAT
N001035.DAT
N63215.DAT
N643418.DAT
N64A010.DAT
N64A410.DAT
N651012.DAT
N651213.DAT
N652215.DAT
N65410.DAT
N658299M.DAT
N658299R.DAT
N65A012.DAT
N663018.DAT
N747A415.DAT
naca0012.DAT
naca4.m
naca4412.DAT
newabb.DAT
NL10414F.DAT
NL10416.DAT
NL11215F.DAT
NL20415.DAT
NLR1.DAT
ONERAM6.DAT
pablo.m
RAE100.DAT
RAE101.DAT
RAE102.DAT
RAE103.DAT
RAE104.DAT
RAE2822.DAT
Rsolver.m
runge.m
SC20010.DAT
SC20012.DAT
SC20406.DAT
SC20410.DAT
SC20412.DAT
SC20414.DAT
SC20518.DAT
SC20606.DAT
SC20610.DAT
SC20612.DAT
SC20614.DAT
SC20706.DAT
SC20712.DAT
SC20714.DAT
SC21006.DAT
SC21010.DAT
solvebl.m
source.m
splf.m
stagnation_point.m
SUPER11.DAT
sy.m
VEZBL32.DAT
VEZCAN.DAT
VEZWLTR.DAT
vortex.m
WILBYB.DAT
WILBYC.DAT
WILBYR.DAT
