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March 26, 2016, 11:48 |
Wind tunnel results
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#1 |
New Member
karthikeyan
Join Date: Aug 2012
Location: India
Posts: 15
Rep Power: 13 |
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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May 19, 2016, 03:39 |
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#2 | |
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Adarsh Tiwari
Join Date: May 2016
Posts: 55
Rep Power: 9 |
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 Regards, Workshop Technologies Quote:
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May 27, 2016, 08:50 |
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#3 |
New Member
Luke
Join Date: Nov 2012
Location: italy
Posts: 24
Rep Power: 13 |
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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