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#1 |
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Guest
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Can anyone let me know if a code is available for designing a supersonic nozzle (convergent-divergent) for accelerating Helium to Mach 2 ? One based on the method of characterisitcs will be best suited i guess.
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#2 |
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Guest
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planar or axisymmetrical?
I have a code that uses the method of charateristics to design a nozzle (with uniform outflow). What is it worth to you? |
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#3 |
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Guest
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thank you twister. though we are presently looking at planar flow situations we will be moving into axial geometreis as well. so anything that you can send will be of much help.
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#4 |
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Guest
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I'm interested in getting a copy of your soft??\It's possible?
Thanks Joe |
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#5 |
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Guest
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Hi,
I am interested in getting the code could you please mail me at apurva.shukla@geind.ge.com Thanks Apurva |
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#6 |
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New Member
Logan Myers
Join Date: Apr 2009
Posts: 3
Rep Power: 5 ![]() |
Hi,
Does anybody have a Matlab code for MOC contour design of an axisymmetric supersonic (Mach 2) nozzle they could send me? Or know where I could get one? Thanks in advance, Logan |
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#7 |
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New Member
xiuxiu
Join Date: Dec 2009
Posts: 10
Rep Power: 4 ![]() |
I need a code for designing a diverging section of a 2-D and 3-D supersonic nozzle and being able to plot it with different numbers of points using methods of charecteristics, please email and let me know if there is a way to get this.
Thanks yazixiu@126.com |
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#8 | |
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New Member
zino
Join Date: Mar 2010
Posts: 23
Rep Power: 4 ![]() |
Quote:
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#9 |
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Member
ali
Join Date: May 2009
Posts: 62
Rep Power: 4 ![]() |
I can do analysis , but can't construct the wall contour , any good document describing the procedure?
Regards |
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#10 |
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New Member
maurizio
Join Date: Apr 2011
Posts: 5
Rep Power: 3 ![]() |
I need a code.PLEASE CONTACT ME OR SEND ME ilperaltaò@hotmail.it
tks |
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#11 |
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New Member
Florent Duchaine
Join Date: Jan 2011
Location: Toulouse, France
Posts: 22
Rep Power: 3 ![]() |
you will maybe find what you are looking for here : http://www.cerfacs.fr/~cfdbib/reposi...CFD_07_142.pdf
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#12 |
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Member
ali
Join Date: May 2009
Posts: 62
Rep Power: 4 ![]() |
Florent, Cant find anything related to nozzle wall contour in the doc.
Regards
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#13 |
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New Member
omer musa
Join Date: Feb 2012
Posts: 6
Rep Power: 2 ![]() |
I need a code for designing a diverging section of a 2-D and 3-D supersonic nozzle and being able to plot it with different numbers of points using methods of charecteristics, please email and let me know if there is a way to get this.
Thanks matrices90@gmail.com |
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#14 |
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Member
Serge A. Suchkov
Join Date: Oct 2011
Location: Moscow, Russia
Posts: 34
Blog Entries: 4
Rep Power: 2 ![]() |
You have a look this matlab code http://www.mathworks.com/matlabcentr...ntent/nozzle.m
__________________
/sbin/modinfo gspca_zc3xx | grep author | cut -d , -f 2 |
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#15 |
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New Member
omer musa
Join Date: Feb 2012
Posts: 6
Rep Power: 2 ![]() |
Thanks dear
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#16 |
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New Member
Jeff Kaith
Join Date: Feb 2012
Posts: 1
Rep Power: 0 ![]() |
I need a code to design and develop 3D supersonic nozzle to mesh it with at least 100 numbers of points for fluid flow modeling
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