pablo

说明：  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.)

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
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.....\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
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.....\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