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[Sponsors] |
February 28, 2002, 02:33 |
airfoil identification
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#1 |
Guest
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Hi,
I have the following information about an airfoil shape: NACA 66 camber height/chord length=0.2 thickness/chord=0.09 Is this a complete definition of a certain airfoil ? Has this airfoil a certain number in the NACA numbering system ? Does someone know a place where to get the coordinates of that airfoil ? Thanks in advance, Mark |
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February 28, 2002, 02:59 |
Errata
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#2 |
Guest
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Hi,
I forgot an additional information about that airfoil shape: NACA mean line a=0.8 Regards, Mark |
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February 28, 2002, 06:28 |
Re: airfoil identification
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#3 |
Guest
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Hi Mark,
Try this book "Theory of wing sections" by Abbott and Von Doenhoff, I think the ISBN is 0486605868. This book has a complete list of coordinates for lots of NACA aerofoils and alot of experimental wind tunnel results. Hope this is of use to you, Mark. |
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February 28, 2002, 07:08 |
Re: airfoil identification
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#4 |
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I have that book, but I can not identify the profil number out my given geometric values. There is a NACA 6-series, but the numbers contain also information about the lift coefficient, but I have only geometric parameters.
Thanks, Mark |
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March 5, 2002, 01:41 |
Re: airfoil identification
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#5 |
Guest
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Hi Mark,
Have a look at the original NACA-report Nr. 824. You can it download from http://naca.larc.nasa.gov/reports/1945/naca-report-824/ There you should find all the necessary information. Best regards Markus |
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