Modeling Characteristics for Volumetric Explosives

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N/A
Agency Tracking Number: 28601
Amount: $70,000.00
Phase: Phase I
Program: SBIR
Awards Year: 1995
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
Combustion Research & Flow
174 North Main Street, Bldg., 3 P.o. Box 1150, Dublin, PA, 18917
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Neeraj Sinha
 (215) 249-9780
Business Contact
Phone: () -
Research Institution
A state of the art computational fluid dynamic methodology is proposed for first-principles-based simulation of detonation in FAE clouds. The approach is based on extensions of well proved and established technology currently in routine use for multiphase, chemically reacting and turbulent solid rocket motor exhaust plume analyses. Latest advances in the modeling of multiphase phenomena from the field of transient, solid propellant interior ballistics are also brought to bear upon the FAE problem. Recent developments in large eddy simulation (LES) of turbulence from the field of high speed jets and transient liquid propellant gun interior ballistics provide a physically realistic approach for representing large scale turbulent structures in FAE clouds. The overall FAE modeling framework is constructed around a well proven, unsteady, three-dimensional, finite-volume, CFD code called CRAFT. CRAFT utilizes a fully implicit, upwind scheme with higher order spatial and temporal accuracy to provide for robust shock capturing without spurious oscillations and good resolution of other embedded discontinuities (e.g. flame fronts, limiting particle streamlines, etc.). The overall modeling framework provides a unique capability for a variety of transient, particulate-laden, combusting flowfields.

* information listed above is at the time of submission.

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