Home > Forums > Software User Forums > ANSYS > FLUENT

How is the reference area of a wing with winglet calculated?

Updated Threads

Reply

Search this Thread

January 29, 2022, 15:56	How is the reference area of a wing with winglet calculated?	#1
adiliqbal New Member Iqbal Join Date: Nov 2021 Location: Islamabad / Beijing Posts: 1 Rep Power: 0	I'm simulating a 3D wing with winglet (on the tip) using ANSYS Fluent. I'm confused about how to calculate the area in reference values section. Please check the attached pictures of my wing model. Top view.jpg View.jpg

February 2, 2022, 21:01		#2
AlexanderZ Senior Member Alexander Join Date: Apr 2013 Posts: 2,363 Rep Power: 34	think of it as two separate wings __________________ best regards ****************************** press LIKE if this message was helpful

Reply

Tags

area, fluent, lift and drag calculation, wing, winglet

« 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
mass flow in is not equal to mass flow out	saii	CFX	12	March 19, 2018 05:21
Simulation of a single bubble with a VOF-method	Suzzn	CFX	21	January 29, 2018 00:58
Error in compiling new drag model	k.farnagh	OpenFOAM Programming & Development	13	May 21, 2016 03:08
error message	cuteapathy	CFX	14	March 20, 2012 06:45
CFX Solver Memory Error	mike	CFX	1	March 19, 2008 07:22

All times are GMT -4. The time now is 20:03.