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STREAMLINE NUMERICS INC

Company Information
Address
3221 NW 13TH ST STE A
GAINESVILLE, FL 32609-2189
United States


https://www.snumerics.com

Information

UEI: YSLNMSL67YC7

# of Employees: 4


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Computationally Efficient Multiphase Flow Simulation Tool for Propulsion Test Technology Components

    Amount: $149,926.00

    This project is geared towards a computationally efficient, robust computational fluid dynamics (CFD) tool for simulating unsteady multiphase flows of critical importance to NASA in their ground and l ...

    SBIRPhase I2022National Aeronautics and Space Administration
  2. Multiphase Hypergolic Combustion Simulation Tool Based on Algebraic VOF and Compressible Flamelet Methodologies

    Amount: $124,996.00

    The innovation proposed is an advanced multiphase hypergolic combustion simulation capability in a computational fluid dynamics (CFD) tool called Loci-STREAM, to improve the understanding of hypergoli ...

    SBIRPhase I2021National Aeronautics and Space Administration
  3. A Fast and Robust PIMPLE-Based Algebraic VOF Method for Two-Phase Compressible Flows

    Amount: $124,923.00

    This project is geared towards a computationally efficient, robust computational fluid dynamics (CFD) tool for simulating unsteady multiphase flows of critical importance to NASA in their ground and l ...

    SBIRPhase I2020National Aeronautics and Space Administration
  4. High Performance Solver for Coupled Cavitation and Fluid-Structure Interaction in Cryogenic Environments

    Amount: $700,972.00

    The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of coupled cavitation and fluid-structure interaction (FSI) in fl ...

    SBIRPhase II2019National Aeronautics and Space Administration
  5. Multiphysics Modeling of Dynamic Combustion Processes Using Pareto-Efficient Combustion Framework

    Amount: $149,955.00

    The objective is to develop zonal multi-physics capability for turbulent combustion simulations. The foundation of the proposed work is a novel Pareto-Efficient Combustion (PEC) framework for fidelity ...

    STTRPhase I2019Department of Defense Air Force
  6. Multiscale Eulerian-Lagrangian Spray Methodology Coupled with Flamelet Models for Liquid Rocket Engine Combustion

    Amount: $124,962.00

    The innovation proposed here is a novel multi-scale coupling methodology implemented in the Loci-STREAM CFD code, for developing a high-fidelity, high-performance multiphase combustion modeling capabi ...

    STTRPhase I2018National Aeronautics and Space Administration
  7. High Performance Solver for Coupled Cavitation and Fluid-Structure Interaction in Cryogenic Environments

    Amount: $124,981.00

    The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of coupled cavitation and fluid-structure interaction (FSI) in fl ...

    SBIRPhase I2018National Aeronautics and Space Administration
  8. High Performance Simulation Tool for Multiphysics Propulsion Using Fidelity-Adaptive Combustion Modeling

    Amount: $749,743.00

    The innovation proposed here is a Pareto-Efficient Combustion (PEC) model for fidelity-adaptive combustion modeling capability implemented into the Loci-STREAM CFD code for use at NASA for simulation ...

    STTRPhase II2018National Aeronautics and Space Administration
  9. Meso-scale Framework for Simulating the Response of Structural Reactive Materials to Shock Loading

    Amount: $749,896.00

    Structural reactive materials (SRMs) or multifunctional energetic materials offer the ability to combine the high energy release rates of traditional high explosives with structural strength.When succ ...

    STTRPhase II2018Department of Defense Air Force
  10. High Performance Simulation Tool for Multiphysics Propulsion Using Fidelity-Adaptive Combustion Modeling

    Amount: $124,995.00

    The innovation proposed here is a fidelity-adaptive combustion model (FAM) implemented into the Loci-STREAM CFD code for use at NASA for simulation of rocket combustion. This work will result in a hig ...

    STTRPhase I2017National Aeronautics and Space Administration
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