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Lift and Drag Coefficient data for NACA 2412 Airfoil |
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January 14, 2011, 23:43 |
Lift and Drag Coefficient data for NACA 2412 Airfoil
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#1 |
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Mahbub Islam
Join Date: Mar 2010
Location: Bangladesh
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Hello
I am trying to find Lift and Drag Coefficient for NACA 2412 airfoil using S-A model. Now I need some standard data of Cd and Cl at different Angle of Attack for this airfoil to validate my results. If anyone have these data please respond here or mail me at mahbub.me.buet@gmail.com. Thank you in advance. |
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January 21, 2011, 14:45 |
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#2 |
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Gregor Seljak
Join Date: Oct 2010
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Hi!
You can find wind tunnel data for lift, drag and moment coefficients for many NACA profiles in I. H. Abbot and A. E. Von Doenhoff, Theory of wing sections. If you are unable to obtain a copy of this book I can send you a screenshot of lift and drag plots. |
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January 21, 2011, 20:01 |
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#3 |
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Mahbub Islam
Join Date: Mar 2010
Location: Bangladesh
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Seljak,
It would be great if you send me a screenshot for NACA 2412. I got a copy of Theory of Wing Section but that is not legible enough. Thank you. |
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January 22, 2011, 16:16 |
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#4 |
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Gregor Seljak
Join Date: Oct 2010
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Oh, I meant screenshot of plots from this book. Unfortunately I don't have any other data.
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January 22, 2011, 20:52 |
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#5 |
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Mahbub Islam
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Can you send me the screen shot of this book please?
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January 26, 2011, 21:23 |
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#6 |
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Tobino
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Dear all,
I am calculating ship resistance in Fluent. anybody can explain for me what and how are equation of Force and Coefficient of force in Fluent Report? any advise is welcome to email : Ducminh207@gmail.com |
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January 27, 2011, 12:09 |
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#7 |
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Mahbub Islam
Join Date: Mar 2010
Location: Bangladesh
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Fundamentals of Aerodynamics by John D Anderson, is a great book for NACA 2412 airfoil data.
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January 28, 2011, 00:59 |
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#8 |
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Tobino
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Thank you very much Mr. Mahbub Islam
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April 11, 2011, 03:28 |
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#9 |
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Homer Jay Simpson
Join Date: Oct 2010
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Hi, GreogorS, can you please send me a screenshot of NACA 0012 and 0015 drag and lift coefficients (for different angles of attack)? really appreciate it, thanks.
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April 11, 2011, 04:26 |
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#10 |
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Mahbub Islam
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"Theory of Wing Sections: Including a Summary of Airfoil Data (Dover Books on Physics) by Ira H. Abbott, A. E. von Doenhoff" is available for free download at www.library.nu
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March 28, 2013, 09:16 |
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#11 |
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and do u have the standard data CI and CD of NACA 2412 in different attack angles now? if u do, and can u send it to me? thank u so much
my Email is liubgs1989@gmail.com |
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May 9, 2013, 09:09 |
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#12 |
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Ali
Join Date: Dec 2012
Location: Turkey
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Hi, GreogorS.
If you still have that book (I. H. Abbot and A. E. Von Doenhoff, Theory of wing sections.) can you please send me a screenshot of NACA 0021 drag and lift coefficients for different angles of attack? I'll be thankful. I just found this link that can help about lift coefficient and drag coefficient for different angles of attacks. http://mac6.ma.psu.edu/VAWT/Sand80-2114.pdf Last edited by mct90; May 9, 2013 at 09:47. Reason: addition |
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May 9, 2013, 11:00 |
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#13 | ||
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Lefteris
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You don't know how to use google search, do you?
Quote:
Quote:
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Lefteris |
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May 13, 2013, 04:59 |
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#14 |
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tb_cfd
Join Date: May 2013
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If you are intrested in the lift and drag coefficients of airfoils you can try "javafoil" (see link below)
http://www.mh-aerotools.de/airfoils/javafoil.htm there it is possible to do variations of the angle of attack and you can export the geometry as a textfile, which you can use for CAD-import. Have fun ;-) |
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May 13, 2013, 07:44 |
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#15 | |
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RZA
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Quote:
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December 12, 2013, 10:30 |
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#16 | |
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Meimei Wang
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Quote:
I need the experimental data 7:1 aspect ratio wing with NACA2412 airfoil, rectangular planar form and no twist as the basis, AoA of 5 degrees. Is it possible to find it anywhere online or from a document like a book? Otherwise I would like to have the experimental data of a similar geometry as the CFD validation. Where to find it?
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Best regards, Meimei |
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December 12, 2013, 10:47 |
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#17 |
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Lefteris
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Try the Theory of Wing Sections by Abbott and von Doenhoff
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Lefteris |
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December 12, 2013, 10:54 |
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#18 |
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Meimei Wang
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Okay. I need to borrow that book from the library. Beforehand, I'm wondering does it include 3D experimental data?
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December 12, 2013, 11:10 |
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#19 |
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Lefteris
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Nope, it has only data for the 2D case but for a huge range of aerofoils.
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Lefteris |
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December 12, 2013, 11:28 |
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#20 |
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Meimei Wang
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Where to find the 3D wing experiment data?
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Best regards, Meimei |
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