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-   -   Code for SUPERSONIC NOZZLE DESIGN (http://www.cfd-online.com/Forums/main/7175-code-supersonic-nozzle-design.html)

Amardip February 17, 2004 18:00

Code for SUPERSONIC NOZZLE DESIGN
 
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.

Twister February 19, 2004 11:22

Re: Code for SUPERSONIC NOZZLE DESIGN
 
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?

Amardip February 19, 2004 15:05

Re: Code for SUPERSONIC NOZZLE DESIGN
 
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.

joe February 19, 2004 16:12

Re: Code for SUPERSONIC NOZZLE DESIGN
 
I'm interested in getting a copy of your soft??\It's possible?

Thanks

Joe

Apurva March 22, 2004 00:59

Re: Code for SUPERSONIC NOZZLE DESIGN
 
Hi,

I am interested in getting the code could you please mail me at apurva.shukla@geind.ge.com

Thanks

Apurva

logan April 14, 2009 13:16

Nozzle code
 
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

hjunjun March 4, 2010 11:42

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

zino February 9, 2011 14:34

MOC code
 
Quote:

Originally Posted by Twister
;27802
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?

anyone found the code?n does it really work? I also need it. please email at faiza_uzma01@yahoo.com

alikami April 26, 2011 00:32

code
 
I can do analysis , but can't construct the wall contour , any good document describing the procedure?
Regards

ilperalta April 26, 2011 10:44

Code
 
I need a code.PLEASE CONTACT ME OR SEND ME ilperaltaņ@hotmail.it
tks

Florent April 27, 2011 03:20

you will maybe find what you are looking for here : http://www.cerfacs.fr/~cfdbib/reposi...CFD_07_142.pdf

alikami April 27, 2011 04:00

contour
 
Florent, Cant find anything related to nozzle wall contour in the doc.
Regards :eek:

omer musa February 3, 2012 04:01

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

SergeAS February 4, 2012 20:16

You have a look this matlab code http://www.mathworks.com/matlabcentr...ntent/nozzle.m

omer musa February 10, 2012 04:04

Thanks dear

cfdanalysis February 10, 2012 09:24

Need code
 
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

abdul Sami February 17, 2013 11:44

c-d nozzle
 
please can any one answer
why static pressure decrease in divergent section of nozzle and ehy total pressure and temperature remain constant througout the nozzle plz plz plz can any answer

Florent February 17, 2013 12:15

Quote:

Originally Posted by abdul Sami (Post 408305)
please can any one answer
why static pressure decrease in divergent section of nozzle and ehy total pressure and temperature remain constant througout the nozzle plz plz plz can any answer

Go back to the Euler equations !

Bdew8556 October 17, 2013 22:17

Designing a con di nozzle
 
Hi guys,

I need to design a nozzle to deliver a set amount of thrust. Apparently I need some kind of code to help me find the nozzle geometry and im drawing a blank.

Does anyone have any code that could help?

Cheers

Brett

lizard_asl May 22, 2014 13:03

Fortran code
 
Does anybody here have a Fortran code for Quasi-One-Dimensional Nozzle Flows? :confused:


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