Streamline Numerics, Inc.

3221 North West 13th Street, Suite A
Gainesville, FL 32609
http://www.snumerics.com
2 Employees

SBIR Award Summary

Total Number of Awards 20
Total Value of Awards $5.98MM
First Award Date 01/01/04
Most Recent Award Date 09/30/15

Key Personnel

Last Name Name Awards Contact
Thakur Dr. Siddharth Thakur 23 Message
Wright Jeffrey Wright 1 Message
Udaykumar H.S. Udaykumar 1 Message
Provided None Provided None Provided None Provided 1

20 Awards Won

Phase 1 STTR

Institution: University of Iowa

Agency: Air Force
Topic: AF15-AT28
Budget: 09/30/15 - 09/30/16

ABSTRACT: 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 initiation of energetic materials in explosives applications depends sensitively on hot-spots that originate from various heterogeneities at the meso ...

Phase 2 STTR

Institution: Stanford University

Agency: National Aeronautics and Space Administration
Topic: T1.01
Budget: 05/26/15 - 05/25/17

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 integrated into Loci-STREAM which is a CFD solver developed by the proposing personnel under funding from NASA over the last several years. A new spray-fla...

Phase 1 STTR

Institution: Stanford University

Agency: National Aeronautics and Space Administration
Topic: 14-1-T1.01
Budget: 01/01/14 - 12/31/14

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 integrated into Loci-STREAM which is a CFD solver developed by the proposing personnel under funding from NASA over the last several years. A new spray-fla...

Phase 2 STTR

Institution: Mississippi State University

Agency: National Aeronautics and Space Administration
Topic: 12-2-T1.01
Budget: 01/01/14 - 12/31/14

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 CFD applications. This project will address critical needs in order to enable fast and accurate simulations of liquid space propulsion systems of ...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 14-1-H2.03
Budget: 01/01/14 - 12/31/14

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 reduced performance, mechanical vibrations, and component erosion. The Computational Fluid Dynamics (CFD) solver Loci-STREAM?developed by Streamline Nu...

Phase 1 STTR

Institution: Mississippi State University

Agency: National Aeronautics and Space Administration
Topic: 12-1-T1.01
Budget: 01/01/12 - 12/31/12

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 applications. This project will address critical needs in order to enable fast and accurate simulations of liquid space propulsion systems (using pr...

Phase 2 SBIR

Agency: Office of the Secretary of Defense
Topic: OSD09-W04
Budget: 08/13/11 - 10/31/13

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 (HEs) under the effects of imposed loads. Designing propulsion devices and munitions for precise operational performance demands comprehensive underst...

Phase 2 STTR

Institution: University of Michigan

Agency: National Aeronautics and Space Administration
Topic: 09-2-T9.01
Budget: 01/01/11 - 12/31/11

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 relevance to NASA (GOX/GH2, LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b...

Phase 1 STTR

Institution: Mississippi State University

Agency: National Aeronautics and Space Administration
Topic: 10-1-T9.01
Budget: 01/01/11 - 12/31/11

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 turbulent, reacting or non-reacting flows involving real or ideal fluids with practically useful turnaround times. The emphasis will be on a major...

Phase 1 SBIR

Agency: Office of the Secretary of Defense
Topic: OSD09-W07
Budget: 06/16/10 - 12/16/10

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-pronged computational approach is proposed that consists of a microscale and a mesoscale formulation, with a tight coupling between the two. The work ...

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