Home > Forums > Software User Forums > ANSYS > FLUENT

Drag coefficient of the 3D aircraft

Updated Threads

Reply

Search this Thread

October 30, 2007, 09:26	Drag coefficient of the 3D aircraft	#1
Pae Guest Posts: n/a	Hi Can any one give me suggestion of what area i should put in reference value. Frontal area of the aircraft or the wetted area? Thank 4 ya help

October 30, 2007, 11:01	Re: Drag coefficient of the 3D aircraft	#2
Chandra Manik Guest Posts: n/a	I believe everything that normal to the flow

Reply

« 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
Drag Coefficient Convergence Problem	John	FLUENT	18	June 24, 2023 09:22
drag coefficient in ansys fluent 12.0	krishna	FLUENT	19	April 12, 2018 00:49
Incorrect Drag and Drag Coefficient for flow over a cylinder	ozzythewise	Main CFD Forum	8	June 13, 2012 06:24
Drag coefficient for parcels in dieselFoam	sebastian_vogl	OpenFOAM Running, Solving & CFD	5	December 31, 2008 12:19
Automotive test case	vinz	OpenFOAM Running, Solving & CFD	98	October 27, 2008 08:43

All times are GMT -4. The time now is 13:01.