Lift and Drag Coefficient data for NACA 2412 Airfoil

mahbub03 · January 14, 2011, 23:43

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.

GregorS · January 21, 2011, 14:45

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.

mahbub03 · January 21, 2011, 20:01

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.

GregorS · January 22, 2011, 16:16

Oh, I meant screenshot of plots from this book. Unfortunately I don't have any other data.

mahbub03 · January 22, 2011, 20:52

Can you send me the screen shot of this book please?

tobino · January 26, 2011, 21:23

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

mahbub03 · January 27, 2011, 12:09

Fundamentals of Aerodynamics by John D Anderson, is a great book for NACA 2412 airfoil data.

tobino · January 28, 2011, 00:59

Thank you very much Mr. Mahbub Islam

homer_j · April 11, 2011, 03:28

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.

mahbub03 · April 11, 2011, 04:26

"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

liubgs · March 28, 2013, 10:16

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

mct90 · May 9, 2013, 09:09

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

Aeronautics El. K. · May 9, 2013, 11:00

You don't know how to use google search, do you?

Quote:

Originally Posted by liubgs

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

Quote:

Originally Posted by mct90

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

tb_cfd · Today, 04:59

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 ;-)

Engr.RZA · Today, 07:44

Quote:

Originally Posted by mahbub03

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.

Look in the Theory of Wing Section by Abbott

January 14, 2011, 23:43	Lift and Drag Coefficient data for NACA 2412 Airfoil	#1
mahbub03 New Member Mahbub Islam Join Date: Mar 2010 Location: Bangladesh Posts: 25 Rep Power: 5	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.

May 9, 2013, 09:09		#12
mct90 New Member Ali Join Date: Dec 2012 Posts: 4 Rep Power: 2	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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January 21, 2011, 14:45		#2
GregorS New Member Gregor Seljak Join Date: Oct 2010 Posts: 19 Rep Power: 4	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.

January 21, 2011, 20:01		#3
mahbub03 New Member Mahbub Islam Join Date: Mar 2010 Location: Bangladesh Posts: 25 Rep Power: 5	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.

January 22, 2011, 16:16		#4
GregorS New Member Gregor Seljak Join Date: Oct 2010 Posts: 19 Rep Power: 4	Oh, I meant screenshot of plots from this book. Unfortunately I don't have any other data.

January 22, 2011, 20:52		#5
mahbub03 New Member Mahbub Islam Join Date: Mar 2010 Location: Bangladesh Posts: 25 Rep Power: 5	Can you send me the screen shot of this book please?

January 26, 2011, 21:23		#6
tobino Member Tobino Join Date: Jan 2011 Location: Osaka,Japan Posts: 33 Rep Power: 4	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

January 27, 2011, 12:09		#7
mahbub03 New Member Mahbub Islam Join Date: Mar 2010 Location: Bangladesh Posts: 25 Rep Power: 5	Fundamentals of Aerodynamics by John D Anderson, is a great book for NACA 2412 airfoil data.

January 28, 2011, 00:59		#8
tobino Member Tobino Join Date: Jan 2011 Location: Osaka,Japan Posts: 33 Rep Power: 4	Thank you very much Mr. Mahbub Islam

April 11, 2011, 03:28		#9
homer_j New Member Homer Jay Simpson Join Date: Oct 2010 Posts: 1 Rep Power: 0	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.

April 11, 2011, 04:26		#10
mahbub03 New Member Mahbub Islam Join Date: Mar 2010 Location: Bangladesh Posts: 25 Rep Power: 5	"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

March 28, 2013, 10:16		#11
liubgs New Member Join Date: Dec 2012 Posts: 2 Rep Power: 0	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

Today, 04:59		#14
tb_cfd New Member tb_cfd Join Date: May 2013 Posts: 1 Rep Power: 0	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 ;-)