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Old   March 26, 2016, 11:48
Default Wind tunnel results
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karthikeyan
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In low Reynold airfoils experimental results are available in Vol 1-5 by selig. In these volumes experimental values are represented as polar plot in chapter 4 or 5 and plotted values in given in appendix E. In polar values given for Re 60,000, 100,000, 150,000. But in appendix values are not matching with former one. which could be taken as reference value?
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Old   May 19, 2016, 03:39
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Adarsh Tiwari
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Hi Karthikeyan,

I don't have access to this book. Kindly share more details so that we can help you better.
We have a proven track record in CAD, CFD, CAE, FEM, Automation, Manufacturing, Web-Design and Digital Marketing. You can see our profile at: http://workshopwale.com and can mail me at: adarsh@workshopwale.com

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In low Reynold airfoils experimental results are available in Vol 1-5 by selig. In these volumes experimental values are represented as polar plot in chapter 4 or 5 and plotted values in given in appendix E. In polar values given for Re 60,000, 100,000, 150,000. But in appendix values are not matching with former one. which could be taken as reference value?
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Old   May 27, 2016, 08:50
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Luke
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for sure the tabs one, instead of pictures, please pay attention on the parameters considered written on and below the table!
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