NASA Technical Reports Server
+ Visit NASA.gov
+ Contact NASA
ABOUT NTRS SEARCH NTRS NTRS NEWS HELP FEEDBACK ORDER NASA INFO.
  + Home
SEARCH NTRS
Navigattion Search Options
Collection > NASA 

Author > Li, D. 
Author > Merkle, C. L. 
Author > Sankaran, V. 

NASA Center > Marshall Space Flight Center 

Publication Year > 2001-2010 > 2004 

Subject > D-F > Fluid Mechanics And Thermodynamics 

Availability Options > Online > PDF 

Item/Media Type > Preprint 


Note: Start a new navigation search by selecting a link above

Image of Earth and the Proteus research aircraft with spiral galaxy in background and the words 'Aerospace Information for a Changing World' Visit the STI Program Web Site
SEARCH NTRS

    Previous Record | Next Record + Back to Results

  + Printer Friendly
Title: Analysis of Regen Cooling in Rocket Combustors
Author(s): Merkle, C. L.; Li, D.; Sankaran, V.
Abstract: The use of detailed CFD modeling for the description of cooling in rocket chambers is discussed. The overall analysis includes a complete three-dimensional analysis of the flow in the regenerative cooling passages, conjugate heat transfer in the combustor walls, and the effects of film cooling on the inside chamber. The results in the present paper omit the effects of film cooling and include only regen cooling and the companion conjugate heat transfer. The hot combustion gases are replaced by a constant temperature wall boundary condition. Load balancing for parallel cluster computations is ensured by using single-block unstructured grids for both fluids and solids, and by using a 'multiple physical zones' to account for differences in the number of equations. Validation of the method is achieved by comparing simple two-dimensional solutions with analytical results. Representative results for cooling passages are presents showing the effects of heat conduction in the copper walls with tube aspect ratios of 1.5:l.
NASA Center: Marshall Space Flight Center
Publication Date: May 13, 2004
Document Source: CASI
Online Source: View PDF File
Document ID: 20040075891
Publication Information: Number of Pages = 8
Contract-Grant-Task Number: NCC8-200
Price Code: A02
Meeting Information: 52nd JANNAF Joint Propulsion Meeting, 10-14 May 2004, Las Vegas, NV, United States
Keywords: COMBUSTION CHAMBERS; THREE DIMENSIONAL MODELS; REGENERATIVE COOLING; HEAT TRANSFER; FILM COOLING; TWO DIMENSIONAL MODELS; COMPUTATIONAL FLUID DYNAMICS; COPPER;
Accessibility: Unclassified; No Copyright; Unlimited; Publicly available;
Updated/Added to NTRS: 2008-06-02

+ Back to Top

USAGov logoExternal Site
+ Sponsored by the NASA Scientific and Technical
   Information Program

+ 2004 Vision for Space Exploration
+ Freedom of Information Act
+ NASA Web Privacy Policy and Important Notices
+ NASA Disclaimers, Copyright Notice,
   and Terms and Conditions of Use


NASA

NASA Official: Calvin Mackey
Page Curator: NASA Center for AeroSpace Information (help@sti.nasa.gov)
Last Updated: July 5, 2007