Home > Forums > General Forums > Main CFD Forum

normal shock keep moving reverse inside intake in supersonic 2 ramp compression intak

Updated Threads

Reply

Search this Thread

November 27, 2023, 05:47	normal shock keep moving reverse inside intake in supersonic 2 ramp compression intak	#1
RIPJAWSKILLS New Member Osama Zahid Join Date: Sep 2023 Posts: 3 Rep Power: 2	I am trying to do a 2D analysis of supersonic intake with 2 ramp angles. the normal shock comes back from the diffuser area to the throat but then continues to move forward when I increase the iteration. using steady, DES with k omega SST. can anyone help in this case. pressure at inlet and outlet are provided. flow is of Mach 2.5

Reply

Tags

inlet, intake aerodynamics, normal shock, oblique shock, supersonic

« 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
supersonic flow past compression ramp	yapalparvi	OpenFOAM Running, Solving & CFD	1	June 14, 2017 11:13
Simulation of moving normal shock wave	ROHAN	Main CFD Forum	1	May 22, 2016 03:14
how can make normal shock in the nozzle at inlet B.C : Pressure Far field	SonicGhoul	FLUENT	2	May 8, 2016 05:16
[snappyHexMesh] determining displacement for added points	CFDnewbie147	OpenFOAM Meshing & Mesh Conversion	1	October 22, 2013 09:53
Will compression waves overtake a moving shock?	GRA	Main CFD Forum	2	October 19, 2006 00:24

All times are GMT -4. The time now is 01:50.