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STREAMLINE NUMERICS, INC.
UEI: YSLNMSL67YC7
# of Employees: 4
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Multi-Scale Simulation Framework for Heterogeneous Energetic Materials
Amount: $1,498,835.00This Phase II STTR proposal will develop a computational tool for state-of-the-art computational modeling of multi-scale thermo-mechanics of heterogeneous energetic materials. The proposal will bring ...
STTRPhase II2017Department of Defense Air Force -
Computation of Structural Energetic Materials Under Shock Loading: a Meso-Scale Framework
Amount: $149,822.00Structural energetic materials or multifunctional energetic materials offer the ability to combine the high energy release rates of traditionalhigh explosives with structural strength. When successful ...
STTRPhase I2016Department of Defense Air Force -
Multi-Scale Simulation Framework for Heterogeneous Energetic Materials
Amount: $149,887.00ABSTRACT: Designing propulsion devices and munitions for precise operational performance demands control and manipulation of energy released by explosive materials. It is well recognized that the init ...
STTRPhase I2015Department of Defense Air Force -
High Fidelity Tool for Turbulent Combustion in Liquid Launch Propulsion Systems Based on Spray-Flamelet Methodology
Amount: $748,058.00The innovation proposed here is a high-performance, high-fidelity simulation capability for simulating liquid rocket spray combustion based on a novel spray-flamelet methodology which will be integrat ...
STTRPhase II2015National Aeronautics and Space Administration -
Advanced Simulation Capability for Turbopump Cavitation Dynamics Guided by Experimental Validation
Amount: $122,041.00Numerical cavitation modeling capability is critical in the design of liquid rocket engine turbopumps, feed lines, injector manifolds and engine test facilities. Cavitation in turbopumps leads to redu ...
SBIRPhase I2014National Aeronautics and Space Administration -
High Fidelity Tool for Turbulent Combustion in Liquid Launch Propulsion Systems Based on Spray-Flamelet Methodology
Amount: $124,145.00The innovation proposed here is a high-performance, high-fidelity simulation capability for simulating liquid rocket spray combustion based on a novel spray-flamelet methodology which will be integrat ...
STTRPhase I2014National Aeronautics and Space Administration -
High Performance Multiphase Combustion Tool Using Level Set-Based Primary Atomization Coupled with Flamelet Models
Amount: $749,611.00The innovative methodologies proposed in this STTR Phase 2 project will enhance Loci-STREAM which is a high performance, high fidelity simulation tool already being used at NASA/MSFC for a variety of ...
STTRPhase II2014National Aeronautics and Space Administration -
High Performance Multiphase Combustion Tool Using Level Set-Based Primary Atomization Coupled with Flamelet Models
Amount: $124,791.00The innovative methodologies proposed in this STTR Phase 1 project will enhance Loci-STREAM which is a high performance, high fidelity simulation tool already being used at NASA for a variety of CFD a ...
STTRPhase I2013National Aeronautics and Space Administration -
Advanced Simulation Framework for the Mesoscale Dynamics of Heterogeneous Explosives
Amount: $1,047,769.00The proposed work seeks to develop a computational tool to conduct sophisticated and realistic computational modeling of the mesoscale dynamics of heterogeneous energetic materials/high explosives (HE ...
SBIRPhase II2012Department of Defense Office of the Secretary of Defense -
Efficient Parallel Solver for Unsteady Flow Physics in Complex Space Propulsion Geometries
Amount: $99,822.00The innovation proposed here is a framework for the incorporation of high performance, high fidelity computational fluid dynamics (CFD) techniques to enable accurate and robust simulation of unsteady ...
STTRPhase I2011National Aeronautics and Space Administration
