Lift and Drag for B737(mid-span)

merthydrglu · April 12, 2018, 18:27

Hi guys, I'm working for analyze Boeing 737 mid-span airfoil. I'm using k-omega SST model. Also, assuming ideal gas with 'sutherland' viscosity. I attached my solution for attack angle with 1.55 degree. I'm not sure my solution is correct and my curiosity is where I can find wind tunnel data(lift, drag coefficient) for comparing with my airfoil.

Gert-Jan · April 13, 2018, 07:12

Try to get an answer on the fluent forum. Not the freelancers forum, unless you want to pay for a detailed answer. If so, then send me a Private Message.

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Calculation of lift and drag coefficients on airfoil	CoolHersheys	OpenFOAM Post-Processing	5	September 27, 2021 06:04
How to calculate lift, drag and lift distribution in Star CCM+?	israelcasillas94	STAR-CCM+	4	November 6, 2020 08:35
wrong SU2 calculation for lift and drag coefficient for NAC4421	mechy	SU2	7	January 9, 2017 05:18
[OpenFOAM] Display lift and Drag in paraview	SamerAli	ParaView	1	May 16, 2013 12:51
Correct lift but wrong pressure drag - possible?	zx	Main CFD Forum	4	July 27, 2007 23:38

April 13, 2018, 07:12		#2
Gert-Jan Senior Member Gert-Jan Join Date: Oct 2012 Location: Europe Posts: 1,827 Rep Power: 27	Try to get an answer on the fluent forum. Not the freelancers forum, unless you want to pay for a detailed answer. If so, then send me a Private Message.