Streamline Numerics, Inc.

Basic Information

3221 North West 13th Street, Suite A
Gainesville, FL, 32609-2189

Company Profile

n/a

Additional Details

Field Value
DUNS: 90574786
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 2


  1. High Performance Multiphase Combustion Tool Using Level Set-Based Primary Atomization Coupled with Flamelet Models

    Amount: $749,611.00

    The 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 ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  2. Advanced Simulation Capability for Turbopump Cavitation Dynamics Guided by Experimental Validation

    Amount: $122,041.00

    Numerical 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 ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  3. High Fidelity Tool for Turbulent Combustion in Liquid Launch Propulsion Systems Based on Spray-Flamelet Methodology

    Amount: $124,145.00

    The 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 ...

    STTR Phase I 2014 National Aeronautics and Space Administration
  4. High Performance Multiphase Combustion Tool Using Level Set-Based Primary Atomization Coupled with Flamelet Models

    Amount: $124,791.00

    The 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 ...

    STTR Phase I 2013 National Aeronautics and Space Administration
  5. Advanced Simulation Framework for the Mesoscale Dynamics of Heterogeneous Explosives

    Amount: $747,990.00

    The 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 ...

    SBIR Phase II 2012 Department of Defense Air Force
  6. Efficient Parallel Solver for Unsteady Flow Physics in Complex Space Propulsion Geometries

    Amount: $99,822.00

    The 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 ...

    STTR Phase I 2011 National Aeronautics and Space Administration
  7. Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems

    Amount: $594,289.00

    The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving propellants of re ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  8. Advanced Simulation Framework for the Mesoscale Dynamics of Heterogeneous Explosives

    Amount: $99,954.00

    The 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 ...

    SBIR Phase I 2010 Department of Defense Air Force
  9. Development and Testing of Advanced Hybrid Energetic Material Systems

    Amount: $99,683.00

    The overall objective of the proposed effort is to advance and test novel design ideas of hybrid explosives and accurately assess their effectiveness in delivering game changing effects. A three-pron ...

    SBIR Phase I 2010 Department of Defense Air Force
  10. Advanced Simulation Framework for Design and Analysis of Space Propulsion Systems

    Amount: $599,438.00

    The innovation proposed here is a high-performance, high-fidelity framework in the computational fluid dynamics (CFD) code called Loci-STREAM to enable accurate, fast and robust simulations of unstead ...

    STTR Phase II 2010 National Aeronautics and Space Administration

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