Home > Forums > General Forums > Main CFD Forum

Validation of axial compressor results

Updated Threads

Reply

Search this Thread

May 6, 2021, 04:36	Validation of axial compressor results	#1
pb123 New Member Pramod Join Date: May 2021 Posts: 1 Rep Power: 0	I intended to use axial compressor blade geometry, NACA 65-1210, however, in journal articles I haven't got compressor map for this blade geometry for the validation purpose. I got the compressor map for NACA 65-306. I have modelled NACA 65-306 blade geometry and validated the same. Now, can I use NACA 65-1210 blade to work on my problem? Or do I have to use NACA 65-306? Kindly provide your opinion.

Reply

Tags

blade & aerofoil, blade geometry, validation

« 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
ActuatorDiskExplicitForce in OF2.1. Help	be_inspired	OpenFOAM Programming & Development	10	September 14, 2018 12:12
Sub-configuration validation: Axial fan	RobV	Main CFD Forum	0	May 2, 2017 13:15
How to calcualte Axial flux of angular momentum and Axial flux of axial momentum ?	nanavati	OpenFOAM Running, Solving & CFD	0	November 21, 2014 10:47
CFX problem in ubuntu (linux)	Vigneshramaero	CFX	0	July 13, 2012 11:22
CFX-Pre problem, pls help!!!	cth_yao	CFX	0	February 17, 2012 01:52

All times are GMT -4. The time now is 22:40.