NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development of a three-phrase combustion code for modeling liquid rocket enginesA two-dimensional/axisymmetric program for the simulation of three-phase reactive flows is presented. The three phases are: a multiple-species gaseous phase, a single-species liquid phase, and a particulate droplet phase. The liquid and gaseous phases are described with continuous Eulerian equations, while the droplets are described in a discrete Lagrangian fashion. The three phases are fully coupled together. An atomization model, a multireaction chemical kinetics model, and a subgrid scale turbulence model completes the description of a general liquid/gas bipropellant combustion process. The code development criteria and qualitative features are highlighted.
Document ID
19850014243
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liang, P. Y.
(Rockwell International Corp. Canoga Park, CA, United States)
Chang, Y. M.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Publication Information
Publication: APL 21st JANNAF Combust. Meeting, Vol. 1
Subject Category
Inorganic And Physical Chemistry
Accession Number
85N22554
Funding Number(s)
CONTRACT_GRANT: NAS8-34928
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available