Streamline Numerics, Inc.
Dba Streamline Numerics Inc
CAGE Code: 1TJS2
NCAGE Code: 1TJS2
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 090574786
Summary
Streamline Numerics, Inc., Dba Streamline Numerics Inc is an Active Commercial Supplier with the Cage Code 1TJS2 and is tracked by Dun & Bradstreet under DUNS Number 090574786..
Address
3221 Nw 13Th St
Ste A
Gainesville FL 32609-2189
United States
Points of Contact
- Telephone:
- 3522718841
- Fax:
- 3522718841
-
http://www.snumerics.com/
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Frequently Asked Questions (FAQ) for CAGE 1TJS2
- What is CAGE Code 1TJS2?
- 1TJS2 is the unique identifier used by NATO Organizations to reference the physical entity known as Streamline Numerics, Inc. Dba Streamline Numerics Inc located at 3221 Nw 13Th St, Ste A, Gainesville FL 32609-2189, United States.
- Who is CAGE Code 1TJS2?
- 1TJS2 refers to Streamline Numerics, Inc. Dba Streamline Numerics Inc located at 3221 Nw 13Th St, Ste A, Gainesville FL 32609-2189, United States.
- Where is CAGE Code 1TJS2 Located?
- CAGE Code 1TJS2 is located in Gainesville, FL, USA.
Contracting History for CAGE 1TJS2 Most Recent 25 Records
- 80NSSC20C0536
- A Fast And Robust Pimple-Based Algebraic Vof Method For Two-Phase Compressible Flows
- 3 Aug 2020
- A Fast And Robust Pimple-Based Algebraic Vof Method For Two-Phase Compressible Flows
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,923.00
- National Aeronautics And Space Administration (Nasa)
- FA930019P1502
- Multiphysics Modeling Of Dynamic Combustion Process Using Pareto-Efficient Combustion Framework
- 24 Jun 2019
- Multiphysics Modeling Of Dynamic Combustion Process Using Pareto-Efficient Combustion Framework
- Fa9300 Aftc Pzr
- Department Of Defense (Dod)
- $149,955.00
- Department Of Defense (Dod)
- 80NSSC21C0334
- Multiphase Hypergolic Combustion Simulation Tool Based On Algebraic Vof And Compressible Flamelet Methodologies. Landing Systems Technologies
- 5 May 2021
- Multiphase Hypergolic Combustion Simulation Tool Based On Algebraic Vof And Compressible Flamelet Methodologies. Landing Systems Technologies
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0334
- Multiphase Hypergolic Combustion Simulation Tool Based On Algebraic Vof And Compressible Flamelet Methodologies. Landing Systems Technologies
- 13 Sep 2021
- Multiphase Hypergolic Combustion Simulation Tool Based On Algebraic Vof And Compressible Flamelet Methodologies. Landing Systems Technologies
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0115
- Eo14042 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)
- 11 Oct 2021
- Eo14042 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)
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $700,972.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC22PB206
- E014042 Phase 1 Computationally Efficient Multiphase Flow Simulation Tool For Propulsion Test Technology Components
- 15 Jul 2022
- E014042 Phase 1 Computationally Efficient Multiphase Flow Simulation Tool For Propulsion Test Technology Components
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- National Aeronautics And Space Administration (Nasa)
- $149,926.00
- National Aeronautics And Space Administration (Nasa)