Home > Forums > Software User Forums > ANSYS > FLUENT

coeffiecnt of lift and drag for naca0012

Updated Threads

Reply

Search this Thread

June 6, 2012, 05:04	coeffiecnt of lift and drag for naca0012	#1
vikramaditya91 New Member eu sou cfd Join Date: Jun 2012 Location: Brazil Posts: 18 Rep Power: 14	hey i am pretty new to this ansys and fluent i am trying to calculate coefficient of lift and drag for different angles of attack. Is it possible that i can import a table/ matrix from excel and ask ansys to calculate for each value of angle of attack? or do i have to do it manually for each angle of attack which is quite monotonous and boring? i am quite new to ANSYS FLUENT. so could you explain in detail?

Reply

Tags

angle of attack, coefficient of lift, coeffiecnt of drag, drag, lift

« Previous Thread | Next Thread »

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 Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Lift and Drag ???	Yogibear	STAR-CCM+	5	November 2, 2023 18:14
[ANSYS Meshing] Lift & Drag Meshing Techniques	tylerplowright	ANSYS Meshing & Geometry	6	May 3, 2012 00:53
lift and drag ceofficient problem	icemaniac178	CFX	6	August 17, 2011 19:40
Lift and Drag Monitor Point Values Converging to Zero	Josh	CFX	24	May 9, 2011 11:38
Correct lift but wrong pressure drag - possible?	zx	Main CFD Forum	4	July 28, 2007 00:38

All times are GMT -4. The time now is 18:52.