Experimental Data Set for NACA0012 for high Re

Ravi_iitm · June 16, 2022, 05:08

Hi Everyone,

It's been two days, I am searching for a dedicated compilation of experimental results for NACA0012 airfoil for high Reynolds number (of the order of 6) to compare my computational result.

If anyone is having any pdf or any web links, please share them. Your help will really be appreciated.

Thank You !

Ravi
Ph.D. Research Scholar
IIT Madras

mluckyw · June 17, 2022, 04:01

I think I have seen it in the book "THEORY OF WING SECTIONS Including a Summary of Airfoil Data" by IRA H. ABBOTT and ALBERT E. VON DOENHOFF. I've checked the book just now there's the data for compressibility effect within Mach number 1+

Aeronautics El. K. · June 29, 2022, 18:02

Quote:

Originally Posted by Ravi_iitm

Hi Everyone,

It's been two days, I am searching for a dedicated compilation of experimental results for NACA0012 airfoil for high Reynolds number (of the order of 6) to compare my computational result.

If anyone is having any pdf or any web links, please share them. Your help will really be appreciated.

Thank You !

Ravi
Ph.D. Research Scholar
IIT Madras

I'm surprised that you haven't found the papers by Ladson yet...

requou · June 30, 2022, 04:17

The following paper gives extensive data for NACA0012 at Re of order 6:

-Harris, C.D. Two-dimensional aerodynamic characteristics of the NACA 0012 aerofoil in the Langley 8 foot transonic pressure tunnel, Tech Rep NASA-TM-81927, NASA, USA, 1981.

It is advised as the most accurate work when considering wind tunnel results for NACA0012 by Mccroskey:

-Mccroskey, W.J. A critical assessment of wind tunnel results for the NACA 0012 aerofoil, Tech Rep, NASA-TM-100019, NASA, USA (1987).

June 16, 2022, 05:08	Experimental Data Set for NACA0012 for high Re	#1
Ravi_iitm New Member Ravi Rana Join Date: Jun 2022 Posts: 1 Rep Power: 0	Hi Everyone, It's been two days, I am searching for a dedicated compilation of experimental results for NACA0012 airfoil for high Reynolds number (of the order of 6) to compare my computational result. If anyone is having any pdf or any web links, please share them. Your help will really be appreciated. Thank You ! Ravi Ph.D. Research Scholar IIT Madras

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June 17, 2022, 04:01		#2
mluckyw Member Chrowale Join Date: Sep 2021 Location: Bandung, Indonesia Posts: 63 Rep Power: 5	I think I have seen it in the book "THEORY OF WING SECTIONS Including a Summary of Airfoil Data" by IRA H. ABBOTT and ALBERT E. VON DOENHOFF. I've checked the book just now there's the data for compressibility effect within Mach number 1+

June 30, 2022, 04:17		#4
requou New Member Join Date: Nov 2019 Posts: 19 Rep Power: 7	The following paper gives extensive data for NACA0012 at Re of order 6: -Harris, C.D. Two-dimensional aerodynamic characteristics of the NACA 0012 aerofoil in the Langley 8 foot transonic pressure tunnel, Tech Rep NASA-TM-81927, NASA, USA, 1981. It is advised as the most accurate work when considering wind tunnel results for NACA0012 by Mccroskey: -Mccroskey, W.J. A critical assessment of wind tunnel results for the NACA 0012 aerofoil, Tech Rep, NASA-TM-100019, NASA, USA (1987).