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Clark Y information
Hello,
I need some information about Clark Y profiles. I found a lot of information like coordinates, but I really need design parameters. Like design lift coefficient, nose radius and trailing edge radius. I would really appreciate your help! Bart |
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Clark Y information
wrote:
Hello, I need some information about Clark Y profiles. I found a lot of information like coordinates, but I really need design parameters. Like design lift coefficient, nose radius and trailing edge radius. I would really appreciate your help! Bart Just for you, Bart. At the bottom of the page. http://www.home.earthlink.net/~cavelamb/parasol.htm you do know how to read it, right? Richard -- (remove the X to email) It's never too late to be the person you might have been. George Elliot |
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Clark Y information
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Clark Y information
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Clark Y information
Thank you all very much for the info. Your comments are very helpful!
Bart On Mar 27, 9:25 am, Philippe Vessaire wrote: wrote: I need some information about Clark Y profiles. I found a lot of information like coordinates, but I really need design parameters. Like design lift coefficient, nose radius and trailing edge radius. I would really appreciate your help! Google : "airfoil data" next Google : Xfoil and you will be happy. -- Volem rien foutre al païs! Philippe Vessaire Ò¿Ó¬ |
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Clark Y information
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Clark Y information
I did get the chart, thanks!
To get the data I need, I assumed a NACA 4412 airfoil, as Stealth Pilot suggested. More information about NACA 4412 is available in textbooks, and because I have very low Reynolds numbers, I have to extrapolate or assume a lot of things. Therefore, the difference in thickness and camber isn't a real problem. Thank you all for your advice and time! Bart On Mar 27, 3:03 pm, cavelamb himself wrote: wrote: Thank you all very much for the info. Your comments are very helpful! Bart On Mar 27, 9:25 am, Philippe Vessaire wrote: wrote: I need some information about Clark Y profiles. I found a lot of information like coordinates, but I really need design parameters. Like design lift coefficient, nose radius and trailing edge radius. I would really appreciate your help! Google : "airfoil data" next Google : Xfoil and you will be happy. -- Volem rien foutre al païs! Philippe Vessaire Ò¿Ó¬ Did you get the chart? -- (remove the X to email) It's never too late to be the person you might have been. George Elliot |
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