Fiscal Year:
1997
Title:
Particle Simulation in Solid Propellant Rocket Exhaust Plumes
Agency / Branch:
DOD / ARMY
Contract:
N/A
Award Amount:
$749,832.00
Abstract:
This Phase I proposal involves initiating the path to properly simulating non-equilibrium multiphase flowfields utilizing advanced numerical techniques. Computational fluid dynamics (CFD) methodology for predicting steady and transient, chemically reacting, two - and three-dimensional, multiphase flowfields has advanced rapidly in recent years. However, the modeling of particulates in these advanced codes is deficient. Current model for the description of particle drag/heat transfer between the gas and dispersed phase, as well as particle/surface boundary conditions, particle-particle interactions, particel-turbulance interactions, and volumetric effects are inadequate for the accurate simulation of "real" flowfields. A systematic approach will be developed where these models will be upgraded and incorporated into an existing multi-phase CFD code with the goal of furthering the state of the art for the analysis of multiphase problems.
Principal Investigator:
Brian J. York
2152499780
Business Contact:
Small Business Information at Submission:
Combustion Research & Flow
174 North Main St, Bldg 3 3 P.o. Box 1150 Dublin, PA 18917
EIN/Tax ID:
232759059
DUNS:
N/A
Number of Employees:
Woman-Owned:
No
Minority-Owned:
No
HUBZone-Owned:
No