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April 14, 2010, 15:00 |
Symmetric NACA Airfoil Lift and Drag Data
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#1 |
New Member
Jerid Hayward
Join Date: Apr 2010
Posts: 2
Rep Power: 0 |
Hello,
My name is Jerid I am new to this blog and fairly new to CFD in general I am a degreed ME and within the last few months I have started to do CFD work. I am having a very hard time finding lift and drag data for symmetric NACA airfoils, namely NACA 0020, NACA 0021, and NACA 0024. I can find coordinates and geometry everywhere but no lift and drag data. Please let me know of a website or book to purchase, etc. |
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April 14, 2010, 15:49 |
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#2 |
Senior Member
Join Date: Jul 2009
Posts: 358
Rep Power: 19 |
This is the classic reference
http://books.google.com/books?id=DPZ...20NACA&f=false You can also try looking for old NACA reports via Google. |
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April 14, 2010, 20:18 |
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#3 |
New Member
Jerid Hayward
Join Date: Apr 2010
Posts: 2
Rep Power: 0 |
Thanks, I checked out the book you recommended and it was good for the NACA airfoils from NACA0006 - NACA0012.
For NACA0012 - NACA0025 I found other data after a lot of searching in a Sandia Lab report. |
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April 15, 2010, 05:59 |
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#4 |
New Member
Mahbub Islam
Join Date: Mar 2010
Location: Bangladesh
Posts: 24
Rep Power: 16 |
I like to suggest you a great site www.wolframalpha.com for any kind of engineering data and problem solving.
Here you get the data of lift coefficient and others for all NACA airfoil series. Hope it will help you. |
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