CFD Online Logo CFD Online URL
Home > Forums > General Forums > Main CFD Forum

Regenerative cooling rocket engine

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Search this Thread Display Modes
Old   November 12, 2003, 07:59
Default Regenerative cooling rocket engine
Posts: n/a
Hi~ there.

I'm studying about regenerative cooling nozzle.

It is divided into 2 parts roughly.

One is combustion part, another is cooling channel part.

It is the cooling channel part that I am interested in

What I know is only that the shape of the cooling channel is the major part.

For example, bifurcated channel has the more efficient than straight rectangular channel in terms of the heat transfer, especially at the nozzle of throat.

So, I'm finding the papers or references about this(bifurcated channel in regenerative cooling nozzle)

I will compute this by Fluent or computer code to know the influence of the channel shape (in terms of the heat transfer and wall temperature)

I'd like to know the empirical results or numerical results in order to compare with my results

Anybody know the information about this? (papers or references)

Or if you have studied about this problem, could you give me a advice?


  Reply With Quote


Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

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

Similar Threads
Thread Thread Starter Forum Replies Last Post
Liquid rocket engine non-premixed combustion model Erik FLUENT 2 November 28, 2013 15:09
Regenerative cooling nozzle. Brian NUMECA 3 September 1, 2005 09:53
rocket engine cip_m FLUENT 2 August 16, 2004 15:50
Regenerative cooling nozzle. Brian Main CFD Forum 0 November 10, 2003 02:11
another question about engine cooling system marivani Main CFD Forum 0 February 2, 2000 12:55

All times are GMT -4. The time now is 01:24.