calculating integral quantities for supersonic nozzle -- CFD Online Discussion Forums

April 26, 2018, 01:20	calculating integral quantities for supersonic nozzle	#1
balkrishan Member Bal Krishan Join Date: Jul 2017 Posts: 43 Rep Power: 8	How to calculate the displacement thickness for CD nozzle flow Main doubt is perpendicular to wall OR the perpendicular to central axis which way will make more sense and why? Last edited by balkrishan; April 27, 2018 at 01:19.

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