CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

Pressure Coefficient around NACA 4412 airfoil

Register Blogs Community New Posts Updated Threads Search

Like Tree1Likes
  • 1 Post By fluid23

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   November 3, 2019, 01:49
Default Pressure Coefficient around NACA 4412 airfoil
  #1
New Member
 
Waliur Rahman
Join Date: Apr 2018
Location: Dhaka,Bangladesh
Posts: 27
Rep Power: 7
Waliur Rahman is on a distinguished road
hi,
I am looking for available experimental and theoretical results for pressure coefficient around NACA 4412 at different angle of attack.Can anyone help me?

Thanks in advance,
Regards,
Waliur Rahman
Waliur Rahman is offline   Reply With Quote

Old   November 6, 2019, 16:49
Default
  #2
Senior Member
 
Matt
Join Date: Aug 2014
Posts: 947
Rep Power: 17
fluid23 is on a distinguished road
https://ntrs.nasa.gov/archive/nasa/c...9930091638.pdf
arjun likes this.
fluid23 is offline   Reply With Quote

Old   November 11, 2019, 06:40
Default
  #3
New Member
 
Waliur Rahman
Join Date: Apr 2018
Location: Dhaka,Bangladesh
Posts: 27
Rep Power: 7
Waliur Rahman is on a distinguished road
Quote:
Originally Posted by fluid23 View Post
thank you so much.
Waliur Rahman is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Multiphase flow - incorrect velocity on inlet Mike_Tom CFX 6 September 29, 2016 01:27
How to calculate the pressure coefficient around an airfoil!? sisi OpenFOAM Running, Solving & CFD 19 December 16, 2014 15:43
Problem with restart solution in shape_optimization.py robyTKD SU2 Shape Design 21 May 29, 2013 09:26
Lift and drag coefficient with strange values for NACA airfoil antonio_ing OpenFOAM Running, Solving & CFD 16 September 13, 2012 12:21
how to create a Airfoil 3D Naca 4412 in Fluent- Ansys? peterpans01 ANSYS 3 March 12, 2012 12:51


All times are GMT -4. The time now is 01:01.