supersonic flow -- CFD Online Discussion Forums

June 13, 2001, 12:54	supersonic flow	#1
ariel narvaez Guest Posts: n/a	mi problema es definir el volumen de calculo necesario para solucionar un problema de un transbordador que entra a la atmosfera a velocidad de dos Mach. My problem is to define the fisic volume necesary to "solucionar" a problem of a transbordator that in to atmosfere a velocity of two Mach

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
back pressure at exit for supersonic flow	BigFrank	FLUENT	6	April 24, 2014 16:13
Probelm with supersonic exhaust to ambient	newj	CFX	2	August 9, 2012 19:01
Boundary Condition at outlet for supersonic flow	Benjamin Zachariah	FLUENT	4	April 23, 2007 00:47
Modeling Bleed in Supersonic Flow	Mohd Yousuf Ali	FLUENT	0	March 17, 2007 04:51
Inviscid Drag at subsonic, subcritical Mach #	Axel Rohde	Main CFD Forum	1	November 19, 2001 13:19

All times are GMT -4. The time now is 04:26.